Datasets:
lid stringlengths 46 95 | short_name stringlengths 3 46 | name stringlengths 3 111 | type stringclasses 5
values | start_date timestamp[ns, tz=UTC]date 1950-01-01 00:00:00 2025-09-04 00:00:00 ⌀ | stop_date timestamp[ns, tz=UTC]date 1966-03-01 00:00:00 2099-12-31 00:00:00 ⌀ | description stringlengths 100 1.68k | target_refs stringlengths 8 1.6k ⌀ | instrument_refs stringlengths 5 458 ⌀ | spacecraft_refs stringlengths 13 131 ⌀ | num_targets int32 0 66 | num_instruments int32 0 28 | num_spacecraft int32 0 6 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
urn:nasa:pds:context:investigation:individual.libs_reference_database | libs_reference_database | Acquisition of a Multi-Parameter LIBS Reference Database of Geological Materials | Individual Investigation | 2015-04-14T00:00:00 | 2022-10-27T00:00:00 | The Mineral Spectroscopy Laboratory at Mount Holyoke College has produced a LIBS spectral library collected on nearly 3000 unique reference targets using four instruments. The purpose of the database is to facilitate high-quality calibration models in future LIBS investigations. | null | mhc.chemlibs; mhc.plibs_z300; mhc.plibs_z903; mhc.superlibs | null | 0 | 4 | 0 |
urn:nasa:pds:context:investigation:mission.apollo_11 | apollo_11 | Apollo 11 | Mission | 1969-07-16T00:00:00 | 1969-07-24T00:00:00 | NASA's Apollo 11 mission was the first crewed lunar landing and moonwalk. While on the lunar surface, astronauts measured moonquakes, collected a sample of solar wind, deployed a laser retroreflector, collected lunar samples, and performed ceremonial duties. | plasma_stream.solar_wind; satellite.earth.moon | pse.a11e | spacecraft.a11e | 2 | 1 | 1 |
urn:nasa:pds:context:investigation:mission.apollo_12 | apollo_12 | Apollo 12 | Mission | 1969-11-14T00:00:00 | 1969-11-24T00:00:00 | The Apollo 12 was the second mission that allowed humans to walk on the Moon. It consisted of the Command and Service Module (CSM) and the Lunar Module (LM). The CSM took images of the surface and communicated with Earth. The LM carried the Astronauts and Apollo Lunar Surface Experiments Package (ALSEP) to the surface. | plasma_stream.solar_wind; satellite.earth.moon | ccig.a12a; pse.a12a; side.a12a; sws.a12a | spacecraft.a12a; spacecraft.a12c; spacecraft.a12l | 2 | 4 | 3 |
urn:nasa:pds:context:investigation:mission.apollo_14 | apollo_14 | Apollo 14 | Mission | 1971-01-31T00:00:00 | 1971-02-09T00:00:00 | The Apollo 14 was the third mission that allowed humans to walk on the Moon. It consisted of the Command and Service Module (CSM) and the Lunar Module (LM). The CSM took images of the surface and communicated with Earth. The LM carried the Astronauts and Apollo Lunar Surface Experiments Package (ALSEP) to the surface. | plasma_stream.solar_wind; satellite.earth.moon | ccig.a14a; cplee.a14a; pse.a14a; side.a14a | spacecraft.a14a; spacecraft.a14c; spacecraft.a14l | 2 | 4 | 3 |
urn:nasa:pds:context:investigation:mission.apollo_15 | apollo_15 | Apollo 15 | Mission | 1971-07-26T00:00:00 | 1971-08-07T00:00:00 | The Apollo 15 was the fourth mission that allowed humans to walk on the Moon. It consisted of the Command and Service Module (CSM) and the Lunar Module (LM). The CSM took images of the surface and communicated with Earth. The LM carried the Astronauts and Apollo Lunar Surface Experiments Package (ALSEP) to the surface. | plasma_stream.solar_wind; satellite.earth.moon | ccig.a15a; hfe.a15a; lsrp.a15l; metriccam.a15c; oms.a15c; pancam.a15c; pse.a15a; side.a15a; sws.a15a | spacecraft.a15a; spacecraft.a15c; spacecraft.a15l; spacecraft.a15s | 2 | 9 | 4 |
urn:nasa:pds:context:investigation:mission.apollo_16 | apollo_16 | Apollo 16 | Mission | 1972-04-16T00:00:00 | 1972-04-27T00:00:00 | The Apollo 16 was the fifth mission that allowed humans to walk on the Moon. It consisted of the Command and Service Module (CSM) and the Lunar Module (LM). The CSM took images of the surface and communicated with Earth. The LM carried the Astronauts and Apollo Lunar Surface Experiments Package (ALSEP) to the surface. | plasma_stream.solar_wind; satellite.earth.moon | lsm.a16a; lsrp.a16l; metriccam.a16c; oms.a16c; pancam.a16c; pse.a16a | spacecraft.a16a; spacecraft.a16c; spacecraft.a16l; spacecraft.a16s | 2 | 6 | 4 |
urn:nasa:pds:context:investigation:mission.apollo_17 | apollo_17 | Apollo 17 | Mission | 1972-12-07T00:00:00 | 1972-12-19T00:00:00 | The Apollo 17 was the sixth mission that allowed humans to walk on the Moon. It consisted of the Command and Service Module (CSM) and the Lunar Module (LM). The CSM took images of the surface and communicated with Earth. The LM carried the Astronauts and Apollo Lunar Surface Experiments Package (ALSEP) to the surface. | plasma_stream.solar_wind; satellite.earth.moon | fuvs.a17c; hfe.a17a; lace.a17a; leam.a17a; lsg.a17a; lspe.a17a; metriccam.a17c; pancam.a17c; sep.a17l; tg.a17l | spacecraft.a17a; spacecraft.a17c; spacecraft.a17l; spacecraft.a17s | 2 | 10 | 4 |
urn:nasa:pds:context:investigation:individual.arecibo_radar_imaging_and_doppler_spectroscopy | arecibo_radar_imaging_and_doppler_spectroscopy | Arecibo Radar Imaging and Doppler Spectroscopy | Individual Investigation | 1963-01-01T00:00:00 | 2020-01-01T00:00:00 | The Arecibo Observatory Planetary Radar system operated from 1963 to 2020, utilizing its 12.6 cm and 70-cm radar systems to study asteroids and planetary surfaces. The investigation includes processed data from Doppler-only spectroscopy and delay-Doppler imaging, primarily focusing on small bodies, but also featuring data from planets and moons. Most of the data was collected after the "Gregorian Upgrade" in the late 1990s, as earlier data was often lost or not preserved. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:observing_campaign.atlas | atlas | Asteroid Terrestrial-impact Last Alert System (ATLAS) | Observing Campaign | 2015-01-01T00:00:00 | null | ATLAS is an asteroid impact early warning system developed by the University of Hawaii and funded by NASA. It consists of four telescopes (Hawaii ×2, Chile, South Africa), which automatically scan the whole sky several times every night looking for moving objects. | null | atlas-chl.0m5.sta1600; atlas-hko.0m5.sta1600; atlas-mlo.0m5.sta1600; atlas-sth.0m5.sta1600 | null | 0 | 4 | 0 |
urn:nasa:pds:context:investigation:other_investigation.astromat_data | astromat_data | Astromaterial Geochemical Data | Other Investigation | 2004-08-13T00:00:00 | null | Initially created in support of PDART efforts by Kerstin Lehnert et al., this investigation is designed to accumulate geochemical data of astromaterials acquired via terrestrial laboratory analyses. Geochemical and geochronology analyses of samples returned by space missions (e.g., HAYABUSA, Stardust, Apollo) are included, as are studies of materials recovered through terrestrial exploration (e.g., observed falls, Antarctic Search for Meteorites expeditions). Future missions with a sample return focus may also be included herein. | dust.dust; satellite.earth.moon | null | null | 2 | 0 | 0 |
urn:nasa:pds:context:investigation:individual.atmospheric_modeling_annex | atmospheric_modeling_annex | Atmospheric Modeling Annex Individual Investigation | Individual Investigation | 2025-09-04T00:00:00 | null | Investigation product for use with the PDS Atmospheres Node (ATM) Atmospheric Modeling Annex (AMA) submissions. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:individual.campbell_venus_radar | campbell_venus_radar | B. Campbell Venus Earth-Based Radar Observations | Individual Investigation | 1988-01-01T00:00:00 | 2020-01-01T00:00:00 | This investigation acquired Earth-based, polarimetric radar image data of Venus using the Arecibo Observatory 12.6-cm (2380 MHz) transmitter in Puerto Rico and receivers at the Arecibo Observatory and Green Bank Telescope in West Virginia. The archive contains maps of radar backscatter from Venus assembled from individual looks collected in observing runs from 1988 to 2020. Those looks are also archived in delay-Doppler format with the PDS, and the documentation for that archive details the data collection steps (https://pds-geosciences.wustl.edu/missions/venus_radar/index.htm). In all but the 2012 dataset, the echoes were transmitted from and received at the Arecibo Observatory. In 2012 the Green Bank Telescope was used as a receiver. For each observing year with Venus close to inferior conjunction, there are multi-look views of the "northern" and "southern" hemispheres, defined with respect to the sub-radar point latitude and longitude during the period. All maps are referenced to a 335 E projection longitude. Each map set contains an image in the opposite-sense circular polarization (OCP, sometimes called "polarized") and one in the same-sense circular polarization (SCP, sometimes called "depolarized"). Spatial sampling is at 1 km per pixel, or about 106 pixels per degree on Venus. The individual looks are normalized to the background noise level such that the OCP and SCP mosaics can be ratioed to obtain the circular polarization ratio (CPR). Offsets of order ten pixels with respect to the Magellan-defined cartographic grid may exist across the images and between observing years. | planet.venus | arecibo.305m.recv_s; arecibo.305m.trans_s; gbo.gbt_100m.4mm_receiver | null | 1 | 3 | 0 |
urn:nasa:pds:context:investigation:mission.bopps | bopps | Balloon Observation Platform for Planetary Science | Mission | 2014-09-25T00:00:00 | 2014-09-26T00:00:00 | The 2014 BOPPS flight launched from Ft. Sumner, New Mexico at 8L20, and achieved and altitude of 130,000 feet, from which it observed the asteroid (1) Ceres and comets C/2013 A1 (Siding Spring) and C/2014 E2 (Jacques). | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:mission.cassini-huygens | cassini-huygens | Cassini-Huygens | Mission | 1997-10-15T00:00:00 | 2017-09-15T00:00:00 | Orbiting the ringed planet Saturn and its numerous moons, the Cassini spacecraft was a keystone of exploration of the Saturnian system and the properties of gaseous planets in our solar system. A joint endeavor of NASA, the European Space Agency, or ESA, and the Italian Space Agency, Cassini launched in 1997 along with ESA's Huygens probe. The spacecraft contributed to studies of Jupiter for six months in 2000 before reaching its destination, Saturn, in 2004 and starting a string of flybys of Saturn's moons. That same year it released the Huygens probe on Saturn's moon Titan to conduct a study of the moon's atmosphere and surface composition. In its second extended mission, Cassini made the first observations of a complete seasonal period for Saturn and its moons, flew between the rings and descended into the planet's atmosphere. | asteroid.2685_masursky; astrophysical.gravitational_waves; dust.dust; planet.earth; planet.jupiter; planet.saturn; planet.venus; planetary_system.solar_system; plasma_stream.solar_wind; satellite.earth.moon; satellite.jupiter.callisto; satellite.jupiter.europa; satellite.jupiter.ganymede; satellite.jupiter.io; satellite.saturn.aegaeon; satellite.saturn.albiorix; satellite.saturn.anthe; satellite.saturn.atlas; satellite.saturn.bebhionn; satellite.saturn.bergelmir; satellite.saturn.bestla; satellite.saturn.calypso; satellite.saturn.daphnis; satellite.saturn.dione; satellite.saturn.enceladus; satellite.saturn.epimetheus; satellite.saturn.erriapus; satellite.saturn.fornjot; satellite.saturn.greip; satellite.saturn.hati; satellite.saturn.helene; satellite.saturn.hyperion; satellite.saturn.hyrrokkin; satellite.saturn.iapetus; satellite.saturn.ijiraq; satellite.saturn.janus; satellite.saturn.kari; satellite.saturn.kiviuq; satellite.saturn.loge; satellite.saturn.methone; satellite.saturn.mimas; satellite.saturn.mundilfari; satellite.saturn.narvi; satellite.saturn.paaliaq; satellite.saturn.pallene; satellite.saturn.pan; satellite.saturn.pandora; satellite.saturn.phoebe; satellite.saturn.polydeuces; satellite.saturn.prometheus; satellite.saturn.rhea; satellite.saturn.siarnaq; satellite.saturn.skathi; satellite.saturn.skoll; satellite.saturn.surtur; satellite.saturn.suttungr; satellite.saturn.tarqeq; satellite.saturn.tarvos; satellite.saturn.telesto; satellite.saturn.tethys; satellite.saturn.thrymr; satellite.saturn.titan; satellite.saturn.ymir; star.alf_vir; star.sun; star.wasp-3 | urn:esa:psa:context:instrument:hp.acp; urn:esa:psa:context:instrument:hp.disr; urn:esa:psa:context:instrument:hp.dwe; urn:esa:psa:context:instrument:hp.gcms; urn:esa:psa:context:instrument:hp.hasi; urn:esa:psa:context:instrument:hp.huygens_hk; urn:esa:psa:context:instrument:hp.ssp; caps.co; cda.co; cirs.co; eng.co; hrd.co; inms.co; issna.co; isswa.co; mag.co; mimi-chems.co; mimi-inca.co; mimi-lemms.co; mimi.co; radar.co; rpws.co; rss.co; uvis.co; vims.co | urn:esa:psa:context:instrument_host:spacecraft.hp; spacecraft.co | 66 | 25 | 2 |
urn:nasa:pds:context:investigation:mission.chandrayaan-1 | chandrayaan-1 | Chandrayaan-1 | Mission | 2008-10-22T00:00:00 | 2009-08-28T00:00:00 | The Chandrayaan-1 was an orbiter and impactor mission to the Moon. It was the first for the Indian Space Research Organisation. It was launched on October 22, 2008. It helped confirmed the presence of water on the Moon. | satellite.earth.moon | m3.ch1-orb; mrffr.ch1-orb | spacecraft.ch1-orb | 1 | 2 | 1 |
urn:nasa:pds:context:investigation:mission.chandrayaan-3 | chandrayaan-3 | Chandrayaan-3 | Mission | 2023-07-14T00:00:00 | null | Chandrayaan 3 is an ISRO (Indian Space Research Organization) mission with the primary objective of putting a lander and rover in the highlands near the south pole of the Moon on 23 August 2023 and demonstrating end-to-end landing and roving capabilities. It will also make a number of scientific measurements on the surface and from orbit. It comprises a lander/rover and a propulsion module. The lander/rover will be similar to the Vikram rover on Chandrayaan 2, with improvements to help ensure a safe landing. It will be carried to lunar orbit by the propulsion module which will remain in orbit around the Moon and act as a communications relay satellite. Chandrayaan-3 launched on 14 July 2023 and landed on the Moon on 23 August 2023. From: https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=2023-098A | satellite.earth.moon | chandrayaan-3_vikram.lra | spacecraft.chandrayaan-3_vikram | 1 | 1 | 1 |
urn:nasa:pds:context:investigation:mission.clps_to_2ab | clps_to_2ab | CLPS Task Order 2AB | Mission | 2024-01-08T00:00:00 | 2024-01-18T00:00:00 | The NASA payload suite on Astrobotic Peregrine Mission 1 was slated to provide some of the first measurements from the surface of the Moon since Apollo, but it did not land on the lunar surface due to an anomaly with the propulsion system. The spacecraft was targeting a landing within Sinus Viscositatis in order to provide complementary and meaningful data to NASA’s Lunar-VISE instrument suite, which will land on the nearby Gruithuisen Domes in 2026. The NASA payloads aboard Astrobotic Peregrine 1 were focusing on characterizing the radiation environment in space and on the surface, volatiles present on or near the surface, and surface temperatures and mineralogy. The payload also included the Laser Retroreflector Array (LRA) which could have enabled precise laser ranging from orbiting spacecraft. Because the Peregrine spacecraft never landed on the Moon, all of the data acquired during the mission occurred in cislunar space. This allowed for measurements of the radiation environment experienced by the spacecraft during the mission as well as measurements of volatiles released by the spacecraft during operations and as a result of the anomaly experienced in the propulsion system. Except for the LRA, all other NASA payloads were powered on at various points and collected science data. | satellite.earth.moon | clps_to_2ab_pll.lets; clps_to_2ab_pll.nirvss; clps_to_2ab_pll.nss; clps_to_2ab_pll.pitms | spacecraft.clps_to_2ab_pll | 1 | 4 | 1 |
urn:nasa:pds:context:investigation:mission.clps_to_2im | clps_to_2im | CLPS Task Order 2IM | Mission | 2024-02-15T00:00:00 | 2024-03-23T00:00:00 | The Intuitive Machines 1 (IM-1, TO2-IM) mission launched a Nova-C lander, called Odyssesus, on Feb 15, 2024. Odyssesus landed on Feb 22, 2024 at (80.13S, 1.44E), about 25km east of the Malapert A crater near the south pole region of the Moon, carrying six NASA payloads and commercial cargo. The scientific objectives of the NASA provided payloads included: studies of plume-surface interactions (SCALPSS), radio astronomy and space weather interactions with the lunar surface (ROLSES), and a laser retroreflector array (LRA). These payloads have archived data in the PDS. Odysseus also carried NASA tech demo payloads to demonstrate precision landing technologies (Navigation Doppler Lidar, NDL), communication and navigation node capabilities (Lunar Node-1, LN-1), and measure the quantity of liquid propellant in micro-gravity environments (Radio Frequency Mass Gauge, RFMG). These payloads have not archived data in the PDS. | satellite.earth.moon | clps_to_2im_ncll.lra; clps_to_2im_ncll.rolses; clps_to_2im_ncll.scalpss | spacecraft.clps_to_2im_ncll | 1 | 3 | 1 |
urn:nasa:pds:context:investigation:mission.clps_to_prime1 | clps_to_prime1 | CLPS Task Order PRIME-1 | Mission | 2025-02-27T00:00:00 | 2025-03-07T00:00:00 | The Intuitive Machines 2 (IM-2, CLPS Task Order TO-Prime 1) mission launched a Nova-C lander, called Athena, on UT February 27, 2025. Athena landed on March 6, 2025 at (84.79S, 29.20E) in the Mons Mouton region in the South Pole region of the Moon. It carried three NASA instruments, and commercial cargo. NASA payloads included the LRA (Laser Retroreflector Array), and the payload suite Prime-1 (Polar Resources Ice Mining Experiment-1). PRIME-1 is a suite of two instruments, the TRIDENT drill (The Regolith Ice Drill for Exploring New Terrain) and MSolo (Mass Spectrometer observing lunar operations). MSolo is designed to identify and quantify volatiles, including those that emanate from the lander, drilling processes, and other payloads conducting operations on the surface. LRA is designed to serve as a fiducial marker of the lander on the lunar surface. MSolo and LRA have archived data in the PDS. The TRIDENT drill, a tech demo designed to demonstrate drilling into the lunar regolith, was unable to complete its science objectives due to the final roughly horizontal orientation of the lander, which prevented the drill from reaching the lunar surface. This payload has not archived data in the PDS. | satellite.earth.moon | clps_to_prime1_athena.lra; clps_to_prime1_athena.msolo | spacecraft.clps_to_prime1_athena | 1 | 2 | 1 |
urn:nasa:pds:context:investigation:mission.comet_sl9-jupiter_collision | comet_sl9-jupiter_collision | Comet D/1993 F2 (Shoemaker-Levy 9) Collision into Jupiter | Mission | 1993-01-01T00:00:00 | 1996-01-01T00:00:00 | The impact of comet D/1993 F2 (Shoemaker-Levy 9), colloquially referred to as "SL9", into the planet Jupiter in July 1994 represented the first time in human history that people had discovered a body in the sky and were able to preict its impact on a planet more than a few seconds in advance. The event was observed by both spacecraft and ground-based observatories around the world. | planet.jupiter; satellite.jupiter.europa; satellite.jupiter.io | urn:esa:psa:context:instrument:iue.lwp; urn:esa:psa:context:instrument:iue.lwr; urn:esa:psa:context:instrument:iue.swp | urn:esa:psa:context:instrument_host:spacecraft.iue; spacecraft.go; spacecraft.hst; spacecraft.vg2 | 3 | 3 | 4 |
urn:nasa:pds:context:investigation:other_investigation.clps | clps | Commercial Lunar Payload Services (CLPS) Initiative | Other Investigation | 2024-01-08T00:00:00 | null | Through the Commercial Lunar Payload Services (CLPS) initiative, NASA is working with several American companies to deliver science experiments and technology demonstrations to the surface of the Moon. Individual NASA CLPS task order awards to US companies cover end-to-end delivery services for NASA sponsored instruments, including payload integration, mission operations, launch from Earth, and either landing on the surface of the Moon or being inserted in lunar orbit. The NASA sponsored instruments flying aboard CLPS landers are selected to advance capabilities for science, exploration or commercial development of the Moon, to scientifically study Earth’s nearest neighbor under the Artemis approach, and to test technologies to support human exploration to the Moon. In addition to the NASA payloads aboard, companies are also encouraged to fly their own instruments, such as lander cameras, as well as commercial payloads. | satellite.earth.moon | clps_to_2ab_pll.lets; clps_to_2ab_pll.nirvss; clps_to_2ab_pll.nss; clps_to_2ab_pll.pitms | spacecraft.clps_to_2ab_pll | 1 | 4 | 1 |
urn:nasa:pds:context:investigation:individual_investigation.lab.hydrocarbon_spectra | lab.hydrocarbon_spectra | Cross Section IR Spectroscopy of Hydrocarbons in Planetary Atmospheres | Individual Investigation | 2018-06-15T00:00:00 | null | Laboratory analysis of hydrocarbon chemistry in analog environments approximating Jupiter, Saturn, and Titan's upper atmospheres. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:mission.deep_space_1 | deep_space_1 | Deep Space 1 | Mission | 1998-10-24T00:00:00 | 2001-12-18T00:00:00 | The Deep Space 1 mission was a "new technology" mission that performed engineering tests of various technologies, including io propulsion and autonomous navigation. It also flew by asteroid (9660) Braille and Comet 19P/Borrelly. | comet.19p_borrelly | ds1.ids; ds1.micas; ds1.pepe | spacecraft.ds1 | 1 | 3 | 1 |
urn:nasa:pds:context:investigation:mission.dscovr | dscovr | Deep Space Climate Observatory (DSCOVR) | Mission | 2015-02-11T00:00:00 | null | The Deep Space Climate Observatory (DSCOVR) mission monitors changes in the solar wind, providing space weather alerts and forecasts or geomagnetic storms that could disrupt power grids, satellites, telecommunications, aviation, and GPS. It orbits at the L1 (Lagrange 1) point between the Earth and the Sun and was launched on February 11, 2015. | planet.earth; planet.jupiter; satellite.earth.moon | dscovr.epic | spacecraft.dscovr | 3 | 1 | 1 |
urn:nasa:pds:context:investigation:mission.deep_space_program_science_experiment | deep_space_program_science_experiment | Deep Space Program Science Experiment | Mission | 1991-11-19T00:00:00 | 1994-05-07T00:00:00 | The Deep Space Program Science Experiment (DSPSE), the first in a series of technology demonstrations by the Ballistic Missile Defense Organization (BMDO) and NASA, was launched in 1994. The spacecraft, called Clementine, was expected to be 'lost and gone forever' after its brief mission, similar to the song it was named after. | satellite.earth.moon | clem1.a-star; clem1.b-star; clem1.hires; clem1.lidar; clem1.lwir; clem1.nir; clem1.rss; clem1.uvvis | spacecraft.clem1 | 1 | 8 | 1 |
urn:nasa:pds:context:investigation:other_investigation.media.dsn | media.dsn | DSN Media Calibration | Other Investigation | 1950-01-01T00:00:00 | 2099-12-31T00:00:00 | The DSN Media Calibration investigation is the set of observations and analyses used by the NASA Deep Space Network (DSN) to develop calibrations for the effects of the ionosphere, troposphere, and local weather on propagation of radio signals between DSN antennas and spacecraft. Although small, these effects are measurable and can change the apparent range to and velocity of spacecraft being tracked by the DSN. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:field_campaign.dd_eldorado_nv_2015 | dd_eldorado_nv_2015 | Dust Devil Field Campaign, Eldorado Playa, Nevada, 2015 | Field Campaign | 2012-01-01T00:00:00 | 2013-01-01T00:00:00 | A dust devil field campaign in Eldorado Playa, Nevada conducted over 2012-2013 by Brian Jackson and Ralph Lorenz. The work was published in JGR in 2015. Terrestrial dust devils serve as planetary analogs to dust devils on Mars. The remote meterological stations used in this study provided pressure and temperature data for dust devil encounters in the desert. In some cases measurements of voltage were also acquired. | planet.earth | no-host.lorenz_met_station | null | 1 | 1 | 0 |
urn:nasa:pds:context:investigation:field_campaign.dd_nnss-nv_2019 | dd_nnss-nv_2019 | Dust Devil Field Campaign, Nevada National Security Site (NNSS), Nevada, 2019 | Field Campaign | 2012-01-01T00:00:00 | 2019-01-01T00:00:00 | A dust devil field campaign at the nuclear test stie at the Nevada National Security Site, Nevada conducted over 2019-2023 by Danny Bowman, et al. The work catalogged terrestrial dust devils to serve as planetary analogs to dust devils on Mars. The remote recording stations, consisting of Hyperion IFS-5000 Series Seismically Decoupled Infrasound Sensors (microbarometers), used in this study provided pressure and temperature data for dust devil encounters in the desert. | planet.earth | no-host.hyperion-ifs3000; no-host.hyperion-ifs5000 | null | 1 | 2 | 0 |
urn:nasa:pds:context:investigation:observing_campaign.earth-based-uranus-stellar-occultations | earth-based-uranus-stellar-occultations | Earth-based Observations of Uranus System Stellar Occultations | Observing Campaign | 1972-03-10T00:00:00 | 2002-07-29T00:00:00 | The observing campaign collects Earth-based observations of Uranus stellar occultations from 1972 to 2002, utilizing various high-speed photometers. It includes early events recorded on strip charts, additional unpublished high-SNR ground observations, and two occultations captured by the Hubble Space Telescope, as well as two using 2D imaging arrays. | planet.uranus; ring.uranus.rings | hst.acs; hst.cos; hst.fgs; hst.foc; hst.fos; hst.hsp; hst.hstacs; hst.nicmos; hst.stis; hst.wfc3; hst.wfpc2; multi-host.generic_ccd_camera; multi-host.generic_gaas_hsp; multi-host.generic_insp_hsp; multi-host.generic_ir_hsp; multi-host.generic_nicmos_ir_camera; multi-host.generic_vis_hsp | spacecraft.hst | 2 | 17 | 1 |
urn:nasa:pds:context:investigation:mission.clipper | clipper | Europa Clipper Mission | Mission | 2024-10-14T00:00:00 | 2034-09-30T00:00:00 | NASA's Europa Clipper spacecraft will perform dozens of close flybys of Jupiter's moon Europa, gathering detailed measurements to investigate whether the moon could have conditions suitable for life. Europa Clipper is not a life detection mission - its main science goal is to determine whether there are places below Europa's surface that could support life. | planet.jupiter; satellite.jupiter.callisto; satellite.jupiter.europa; satellite.jupiter.ganymede | clipper.ecm; clipper.eth; clipper.gnc; clipper.mas; clipper.mis; clipper.nac; clipper.pim; clipper.rea; clipper.rss; clipper.sud; clipper.uvs; clipper.wac | spacecraft.clipper | 4 | 12 | 1 |
urn:nasa:pds:context:investigation:mission.clps_to_19d | clps_to_19d | Firefly Aerospace's Blue Ghost Mission 1 | Mission | 2025-01-15T00:00:00 | 2025-03-16T00:00:00 | As part of NASA’s CLPS (Commercial Lunar Payload Services) initiative and Artemis campaign, Firefly’s Blue Ghost lunar lander delivered ten NASA science and technology instruments to Mare Crisium on the near side of the Moon. The CLPS name for the delivery is CLPS Task Order (TO) 19D and the Firefly Aerospace mission name is Blue Ghost Mission 1. Blue Ghost Mission 1 (BGM1) launched on Jan 15, 2025 and landed on March 2, 2025. The surface mission extended through one lunar day and multiple hours into the lunar night before concluding on March 16, 2025. | satellite.earth.moon | clps_to_19d_bgl.lister; clps_to_19d_bgl.lms; clps_to_19d_bgl.lpv; clps_to_19d_bgl.rac; clps_to_19d_bgl.rac.a_bottom; clps_to_19d_bgl.rac.a_top; clps_to_19d_bgl.rac.b_bottom; clps_to_19d_bgl.rac.b_top; clps_to_19d_bgl.radpc; clps_to_19d_bgl.scalpss; clps_to_19d_bgl.scalpss.lfl0; clps_to_19d_bgl.scalpss.lfl1; clps_to_19d_bgl.scalpss.sfl0; clps_to_19d_bgl.scalpss.sfl1; clps_to_19d_bgl.scalpss.sfl2; clps_to_19d_bgl.scalpss.sfl3 | spacecraft.clps_to_19d_bgl | 1 | 16 | 1 |
urn:nasa:pds:context:investigation:individual.frankenspectra | frankenspectra | Frankenspectra Database | Individual Investigation | 2018-02-15T00:00:00 | 2023-04-13T00:00:00 | The purpose of this investigation was to analyze, using reflectance spectroscopy, 27 fine-particulate (less than 10-um) terrestrial minerals to create a far-UV through MIR single spectrum built from the best pieces of spectra acquired at different U.S. and international labs (i.e., Frankenspectra). Multiple-laboratory spectral comparisons increased confidence in determining both better spectral shapes and overall representative reflectance values by considering the reflectance data of each sample as an ensemble. The four laboratories used to acquire the fine-particulate reflectance spectra included the University of Colorado Laboratory for Atmospheric and Space Physics (LASP, Boulder, CO), the Planetary Science Institute (PSI, Tucson, AZ), the University of Winnipeg's Centre for Terrestrial and Planetary Exploration (C-Tape) Planetary Spectrophotometer Facility (UW, Manitoba, Canada), and the Planetary Emissivity Laboratory (PEL, that performs reflectance measurements as well as emissivity) at the German Aerospace Center (Deutsches Land und Raumfahrt, DLR) in Berlin, Germany. | null | lasp.mcpherson-vuvas; pgl.asd-fieldspec3; pgl.ocean_optics-uvflame; psf.asd-labspec4; psl.bruker-vertex80v | null | 0 | 5 | 0 |
urn:nasa:pds:context:investigation:mission.galileo | galileo | Galileo | Mission | 1977-10-01T00:00:00 | 2003-09-21T00:00:00 | The Galileo was sent to Jupiter to study the planet and its moons. It was delivered to space on Space Shuttle Atlantis on October 18, 1989. It sent an atmospheric probe into Jupiter's atmosphere to study the composition. | asteroid.243_ida; asteroid.951_gaspra; calibrator.calibration; planet.earth; planet.jupiter; planet.venus; planetary_system.solar_system; plasma_stream.solar_wind; satellite.earth.moon; satellite.jupiter.amalthea; satellite.jupiter.callisto; satellite.jupiter.europa; satellite.jupiter.ganymede; satellite.jupiter.io | go.epd; go.gdds; go.hic; go.mag; go.nims; go.pls; go.ppr; go.pws; go.rss; go.ssd; go.ssi; go.uvs; gp.asi; gp.dwe; gp.epi; gp.gpms; gp.had; gp.lrd; gp.nep; gp.nfr | spacecraft.go; spacecraft.gp | 14 | 20 | 2 |
urn:nasa:pds:context:investigation:other_investigation.geodesy | geodesy | Geodesy | Other Investigation | null | 2099-12-31T00:00:00 | Geodesy is the scientific field focused on accurately measuring and understanding the Earth's shape, orientation, and gravity. Pythagoras and Eratosthenes made early contributions, with Pythagoras suggesting a spherical Earth and Eratosthenes estimating its circumference. Modern understanding recognizes that the Earth's shape is influenced by various forces, including gravity, rotation, tides, plate tectonics, volcanism, and fluid motion. These factors are continually measured and modeled for historical analysis and predictions. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:individual.goldstone_raw_radar | goldstone_raw_radar | Goldstone Raw Radar | Individual Investigation | 1958-01-01T00:00:00 | null | The Goldstone Solar System Radar (GSSR) is the world's only fully steerable radar capable of high-resolution ranging and imaging of planetary and small-body targets. It enables scientific research on the Moon, planets, and near-Earth objects (NEOs) by providing data on images, topography, surface characteristics, shapes, compositions, and liquid or ice distributions. The radar records complex base-band samples using various receivers, transmitting right circular polarized light while receiving both left and same-sense circular polarizations. The raw data collected can be analyzed to produce frequency spectra or delay-Doppler image maps based on the transmitted waveforms. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:mission.gravity_recovery_and_interior_laboratory | gravity_recovery_and_interior_laboratory | Gravity Recovery and Interior Laboratory | Mission | 2011-09-10T00:00:00 | 2012-12-18T00:00:00 | Gravity Recovery and Interior Laboratory (GRAIL) consist of two small spacecrafts (GRAIL A [Ebb] and B [Flow]). It was launched on September 10, 2011. It used high-quality gravitational field mapping of the Moon to determine its interior structure. On August 31, 2012, the two spacecrafts started collecting data at a lower altitude. | satellite.earth.moon | grail-a.lgrs-a; grail-b.lgrs-b | spacecraft.grail-a; spacecraft.grail-b | 1 | 2 | 2 |
urn:nasa:pds:context:investigation:other_investigation.hot_ion_atmos_escape | hot_ion_atmos_escape | Hot Ion Atmospheric Escape Cross Section Data | Other Investigation | 2015-03-17T00:00:00 | null | Initially started as part of the PDART 2014 efforts of Robert Johnson, this investigation is designed to collate results of modeling and laboratory work in atmospheric escape studies. Data associated with this project include cross section tables for different atmospheric species representing different chemical reactions occuring in the upper atmosphere of planets. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:mission.hst | hst | HST | Mission | 1990-04-08T00:00:00 | null | The Hubble Space Telescope is a cooperative program of the European Space Agency (ESA) and the National Aeronautics and Space Administration (NASA) to operate a long-lived space-based observatory for the benefit of the international astronomical community. HST is an observatory first dreamt of in the 1940s, designed and built in the 1970s and 80s, and launched in the 1990s. HST was designed to be a different type of mission for NASA: a permanent space-based observatory. HST is a 2.4-meter, f/24 Ritchey-Chretien reflecting telescope capable of performing observations in the visible, near-ultraviolet, and near-infrared. It was deployed in low-Earth orbit (600 kilometers altitude) by the crew of the space shuttle Discovery (STS-31) on 25 April 1990. It was visited by astronauts for servicing missions five times, most recently in 2009. | dwarf_planet.134340_pluto; planet.jupiter; planet.mars; planet.mercury; planet.neptune; planet.saturn; planet.uranus; planet.venus; satellite.saturn.dione; satellite.saturn.enceladus; satellite.saturn.epimetheus; satellite.saturn.helene; satellite.saturn.hyperion; satellite.saturn.janus; satellite.saturn.mimas; satellite.saturn.pandora; satellite.saturn.prometheus; satellite.saturn.rhea; satellite.saturn.tethys; satellite.saturn.titan | hst.acs; hst.cos; hst.fgs; hst.foc; hst.hsp; hst.hstacs; hst.nicmos; hst.stis; hst.wfc3; hst.wfpc2 | spacecraft.hst | 20 | 10 | 1 |
urn:nasa:pds:context:investigation:mission.insight | insight | InSight Lander | Mission | 2018-05-05T00:00:00 | 2022-12-15T00:00:00 | NASA's InSight Lander mission placed a lander on Mars that deployed a seismometer and a heat-flow probe, along with cameras, a magnetometer, a meteorology experiment, and a radio science experiment. | planet.mars | apss-ifg.insight; apss-ps.insight; apss-twins.insight; edl.insight; hp3.insight; icc.insight; ida.insight; idc.insight; radiometer.insight; rise.insight; seis.insight | spacecraft.insight | 1 | 11 | 1 |
urn:nasa:pds:context:investigation:individual.lab_shocked_feldspars | lab_shocked_feldspars | Investigation of Laboratory Shocked Feldspars | Individual Investigation | 2015-01-01T00:00:00 | 2019-01-01T00:00:00 | This investigation consists of data acquired from thin sections created from a suite of experimentally shocked plagioclase feldspars (associated with Jaret et al., 2018), and a basalt and basaltic andesite (associated with Johnson et al., 2020). The data products comprise (1) micro-Fourier Transform Infrared (FTIR) thermal infrared hyperspectral image cubes; (2) thermal infrared point spectra acquired with two different detectors (for the plagioclase samples only); (3) micro-Raman spectra; (4) microscope images of the thin sections in plane polarized and cross polarized light; and (5) microscope images of the locations of the Raman and thermal infrared point spectra. The thermal infrared and Raman spectroscopy demonstrate changes as a function of shock pressure, as detailed in Jaret et al., 2018 and Johnson et al., 2020. | null | sbu_cpex.ftir; sbu_cpex.raman | null | 0 | 2 | 0 |
urn:nasa:pds:context:investigation:mission.juno | juno | Juno | Mission | 2011-08-05T00:00:00 | null | Juno is a spacecraft that was launched on August 5, 2011 and arrived at Jupiter in July 2016. Juno is orbiting Jupiter and its prime mission was 32 high inclination, high eccentricity orbits of the planet, acquiring data at each periapsis for several hours. Juno has been taking measurements to help finding clues about how the planet formed, its composition, including its rocky core, and its atmospheric structure and turbulences. The mission was extended for an additional 40 orbits that should continue until September 2025. These orbits have shorter periods, going from ~43 days to ~38 days, and currently at ~33 days. The reduction in the orbial periods allows Juno to conduct close flybys of Ganymede, Europa, Io, and Jupiter's ring system, as well as gather more information about Jupiter's northern hemisphere. | dust.dust; planet.earth; planet.jupiter; planetary_system.solar_system; plasma_stream.solar_wind; satellite.earth.moon; satellite.jupiter.callisto; satellite.jupiter.europa; satellite.jupiter.ganymede; satellite.jupiter.io | fgm.jno; jade.jno; jedi.jno; jiram.jno; jno.rss; junocam.jno; mwr.jno; sru.jno; uvs.jno; waves.jno | spacecraft.jno | 10 | 10 | 1 |
urn:nasa:pds:context:investigation:mission.kaguya | kaguya | Kaguya | Mission | 2007-09-14T00:00:00 | 2009-06-10T00:00:00 | SELENE, Japan's second lunar probe, was renamed Kaguya (Moon Princess) after launch following a public poll. Its mission aimed to orbit the Moon and gather data on its origins, geological evolution, and surface environment, while also conducting radio science experiments. The mission included two small sub-satellites, originally named Relay Satellite (Rstar) and VRAD satellite (Vstar), which were renamed Okina and Ouna, meaning "honorable elderly man" and "honorable elderly woman." | satellite.earth.moon | kaguya.grs; kaguya.lism | spacecraft.kaguya | 1 | 2 | 1 |
urn:nasa:pds:context:investigation:observing_campaign.mcmath-pierce_mercury | mcmath-pierce_mercury | KPNO McMath-Pierce Solar Telescope Observations of Mercury | Observing Campaign | 2010-01-01T00:00:00 | 2011-01-01T00:00:00 | This observing campaign collates obervations of Mercury collected from the McMath-Pierce Solar Telescope at Kitt Peak contemporaneous with MESSENGER's presence at Mercury. | planet.mercury | null | null | 1 | 0 | 0 |
urn:nasa:pds:context:investigation:observing_campaign.lowell_uranus-neptune-photometry | lowell_uranus-neptune-photometry | Lowell Observatory Uranus-Neptune Photometry | Observing Campaign | 1972-01-17T00:00:00 | 2016-10-05T00:00:00 | This observing campaign collates photometric observations of Uranus and Neptune (1972-2016) in the b (472 nm) and y (551 nm) filters of the Strömgren photometric system at Lowell Observatory. Observations recorded mainly seasonal variations of disk-integrated albedos of these objects. This bundle includes 360 observations of Uranus and 433 observations of Neptune from 1972-2016. The work was led by Wes Lockwood from Lowell Observatory. | planet.neptune; planet.uranus | null | null | 2 | 0 | 0 |
urn:nasa:pds:context:investigation:mission.ladee | ladee | Lunar Atmosphere and Dust Environment Explorer (LADEE) | Mission | 2013-09-01T00:00:00 | 2014-02-17T00:00:00 | The Lunar Atmosphere and Dust Environment Explorer (LADEE) was a robotic mission that, from low lunar orbit, gathered detailed information about the lunar atmosphere, conditions near the surface and environmental influences on lunar dust. LADEE was launched in September 2013 and carried out lunar orbital operations for 223 days, concluding when the spacecraft was decommissioned by impact into the moon in April 2014. | satellite.earth.moon | ladee.ldex; ladee.nms; ladee.uvs | spacecraft.ladee | 1 | 3 | 1 |
urn:nasa:pds:context:investigation:mission.lunar_crater_observation_and_sensing_satellite | lunar_crater_observation_and_sensing_satellite | Lunar Crater Observation and Sensing Satellite | Mission | 2009-06-18T00:00:00 | 2009-10-09T00:00:00 | LCROSS launched as a secondary payload with Lunar Reconnaissance Orbiter (LRO) on June 18, 2009. After trans-lunar injection, LRO separated and performed its mission. The LCROSS Shepherding Spacecraft (SSC) remained attached to the spent Atlas upper stage, called the Centaur. Over 112 days, the Shepherding Spacecraft adjusted the Centaur's course to bring it to an impact within the Cabeus Crater near the South Pole of the moon. It impacted on October 9, 2009. LCROSS used the Centaur as a 2300 kg kinetic impactor with more than 200 times the energy of the Lunar Prospector (LP) impact to excavate more than 250 metric tons of lunar regolith. The resulting ejecta cloud was observed from a number of Lunar-orbital and Earth-based assets, and the LCROSS spacecraft. After releasing the Centaur, the SSC flew toward the impact plume, sending real-time data to characterize the morphology, evolution and composition of the plume with a suite of cameras and spectrometers. The SSC then became a 700 kg impactor itself, providing a second opportunity to study the nature of the Lunar Regolith. | urn:nasa:pds:context:instrument:vsp.lcross; satellite.earth.moon | apache_point.arc3m5.agile; magdalena_ridge.mro2m4.photdoc_camera; magdalena_ridge.mro2m4.photgjon_camera; mir1.lcross; mir2.lcross; mmt.single_mirror6m5.ccd47; mmt.single_mirror6m5.clio; nir1.lcross; nir2.lcross; nsp1.lcross; nsp2.lcross; tlp.lcross; vis.lcross; vsp.lcross | spacecraft.lcross | 2 | 14 | 1 |
urn:nasa:pds:context:investigation:mission.lunar_prospector | lunar_prospector | Lunar Prospector | Mission | 1998-01-06T00:00:00 | 1999-07-31T00:00:00 | The Lunar Prospector (LP) Mission consisted of a spin-stabilized orbiter spacecraft designed to perform continuous mapping of the Moon from a circular polar orbit. The LP spacecraft was launched on January 7, 1998 (UTC). The primary mapping mission began on January 16, 1998 and lasted for one year. During most of the mapping mission, the spacecraft mapped the surface from a 118-minute, circular, polar orbit 100 km above the moon's surface. Starting on December 19, 1998, the spacecraft was maneuvered into a 40 km orbit as a transition into a low altitude extended mission orbit. The transition orbit was used to collect gravity data in order to verify the moon's gravity model in preparation for conducting the extended mission orbit. The extended mission began on January 16, 1999. The objective of the extended mission was to provide higher resolution mapping from a circular, polar orbit averaging 30 km above the moon's surface. The Lunar Prospector mission ended on July 31, 1999 when the spacecraft was intentionally impacted into a crater near the south pole. The impact site was targeted for one of the hydrogen deposits detected by Lunar Prospector's Neutron Spectrometer. | satellite.earth.moon | lp.aps; lp.eng; lp.er; lp.grs; lp.mag; lp.mager; lp.ns; lp.rss | spacecraft.lp | 1 | 8 | 1 |
urn:nasa:pds:context:investigation:mission.lunar_reconnaissance_orbiter | lunar_reconnaissance_orbiter | Lunar Reconnaissance Orbiter | Mission | 2009-06-18T00:00:00 | null | The Lunar Reconnaissance Orbiter (LRO), launched on June 18, 2009, continues to orbit and investigate the Moon. The mission objectives include producing a high-resolution global topographic model, mapping the distribution of hydrogen, and identifying lunar landing sites and associated hazards. | satellite.earth.moon | lro.crat; lro.dlre; lro.lamp; lro.lend; lro.lola; lro.lroc; lro.mrflro; lro.rss | spacecraft.lro | 1 | 8 | 1 |
urn:nasa:pds:context:investigation:individual.lunar_simulants_fuv_reflectance_gimar_22 | lunar_simulants_fuv_reflectance_gimar_22 | Lunar Simulants JSC-1A and LMS-1 Far-ultraviolet Reflectance Data Bundle | Individual Investigation | 2017-11-20T00:00:00 | 2021-09-15T00:00:00 | This data bundle contains all of the data presented in the paper "Far-Ultraviolet Photometric Characteristics of JSC-1A and LMS-1 Lunar Regolith Simulants: Comparative Investigations With Apollo 10084" as published in Volume 127, Issue 11 of the Journal of Geophysical Research: Planets. The purpose of this study was to measure the far-ultraviolet (FUV) reflectance properties of the lunar simulants JSC-1A and LMS-1 and compare these properties to those found for the Apollo 11 soil sample 10084 (published previously by U. Raut et al.). Comparing the FUV reflectance of these two simulants and the lunar soil sample provided an opportunity to disentangle the potential contributions of mineralogy and space weathering to lunar soil FUV reflectance. This study's results indicated that titanium-bearing mineral content strongly affects the overall brightness of these soils in the FUV, while space weathering features may correlate to differences in the scattering anisotropy of the soils. | null | swri.swurc; utsa_kamc.bruker_eds; utsa_kamc.hitachi_sem | null | 0 | 3 | 0 |
urn:nasa:pds:context:investigation:mission.lunar_trailblazer | lunar_trailblazer | Lunar Trailblazer | Mission | 2025-02-01T00:00:00 | null | Lunar Trailblazer is a NASA SIMPLEX mission to acquire simultaneous, nested high-resolution near-infrared spectral images and thermal infrared data. The payload consists of the High-resolution Volatiles and Minerals Moon Mapper (HVM3) and the Lunar Thermal Mapper (LTM). The mission will study the mineralogy of the lunar surface at all latitudes, including within Permanently Shadowed Regions. | satellite.earth.moon | lt.hvm3; lt.ltm | spacecraft.lt | 1 | 2 | 1 |
urn:nasa:pds:context:investigation:mission.magellan | magellan | Magellan | Mission | 1989-05-04T00:00:00 | 1994-10-12T00:00:00 | Magellan is a spacecraft that was sent to Venus to study the surface of the planet. It was launched on May 4, 1989 by the Space Shuttle Atlantis. It mapped the surface by radar. | planet.venus | mgn.rdrs; mgn.rss | spacecraft.mgn | 1 | 2 | 1 |
urn:nasa:pds:context:investigation:mission.mariner_10 | mariner_10 | Mariner 10 | Mission | 1973-11-03T00:00:00 | 1975-03-24T00:00:00 | Mariner 10 is a spacecraft launched on November 3, 1973, that conducted flybys of Mercury and Venus. It was the first spacecraft to utilize gravity assist for its journey. | planet.mercury; planet.venus; plasma_stream.solar_wind | m10.mag; m10.pls | spacecraft.m10 | 3 | 2 | 1 |
urn:nasa:pds:context:investigation:mission.mariner67 | mariner67 | Mariner 67 | Mission | 1967-06-14T00:00:00 | 1968-11-05T00:00:00 | The Mariner 67 mission, consisting of the Mariner 5 spacecraft, flew by Venus on 19 October 1967 at an altitude of 4094 km. It returned data data on both interplanetary and Venusian magnetic fields, charged particles, and plasmas, as well as radio refractivity and UV emissions of the Venusian atmosphere. Contact was lost on 7 December, and operations ended 5 November 1968. | planet.venus; plasma_stream.solar_wind | mr5.mag | spacecraft.mr5 | 2 | 1 | 1 |
urn:nasa:pds:context:investigation:mission.mariner69 | mariner69 | Mariner 69 | Mission | 1969-02-24T00:00:00 | 1970-12-28T00:00:00 | The Mariner 69 mission involved two uncrewed NASA spacecraft, Mariner 6 and Mariner 7, which completed the first dual mission to Mars in 1969 under the Mariner program. Mariner 6 launched from Launch Complex 36B and Mariner 7 from Launch Complex 36A at Cape Canaveral Air Force Station. Both spacecraft flew over Mars' equator and south polar regions, analyzing the atmosphere and surface using remote sensors. They recorded and relayed hundreds of images back to Earth. The mission aimed to study Mars' surface and atmosphere during close flybys, laying the groundwork for future investigations, particularly the search for extraterrestrial life. Additionally, it aimed to develop and demonstrate technologies needed for future Mars missions. Mariner 6 also provided valuable experience and data to aid the Mariner 7 encounter five days later. | planet.mars | irs.mr6; irs.mr7; nac.mr6; nac.mr7; uvs.mr6; uvs.mr7; wac.mr6; wac.mr7 | spacecraft.mr6; spacecraft.mr7 | 1 | 8 | 2 |
urn:nasa:pds:context:investigation:mission.mars2020 | mars2020 | Mars 2020: Perseverance Rover | Mission | 2020-07-30T00:00:00 | null | The Mars 2020 Perseverance Rover searches for signs of ancient microbial life, to advance NASA's quest to explore the past habitability of Mars. The rover is collecting core samples of Martian rock and soil (broken rock and soil), for potential pickup by a future mission that would bring them to Earth for detailed study. | planet.mars | mars2020.ecam; mars2020.edlcam; mars2020.helicam; mars2020.lcam; mars2020.mastcamz; mars2020.meda; mars2020.moxie; mars2020.pixl; mars2020.rimfax; mars2020.rover; mars2020.sherloc; mars2020.supercam | spacecraft.mars2020 | 1 | 12 | 1 |
urn:nasa:pds:context:investigation:mission.maven | maven | Mars Atmosphere and Volatile EvolutioN | Mission | 2013-11-13T00:00:00 | null | The Mars Atmosphere and Volatile Evolution (MAVEN) spacecraft was sent to Mars to study the atmosphere. It was launched on November 18, 2013. It would study the loss of volatiles, current state of the upper atmosphere, rate of escape for the gases, and ratios of stable isotopes. In 2017, the orbit was changed to be part of the communications relay for Mars. | planet.mars | acc.maven; euv.maven; iuvs.maven; lpw.maven; mag.maven; ngims.maven; rss.maven; sep.maven; static.maven; swea.maven; swia.maven | spacecraft.maven | 1 | 11 | 1 |
urn:nasa:pds:context:investigation:mission.mars_exploration_rover | mars_exploration_rover | Mars Exploration Rovers: Spirit and Opportunity | Mission | 2000-05-08T00:00:00 | 2019-02-13T00:00:00 | NASA's twin rovers, Spirit and Opportunity, landed on Mars on Jan. 3 and Jan. 24, 2004 PST (Jan. 4 and Jan. 25 UTC), respectively. The rovers were planned as 90-day missions to search for geological clues regarding environmental conditions on early Mars, and assess whether those environments were conducive to life. Spirit lasted 20 times longer than its original design, concluding its mission on March 22, 2010. Opportunity worked for nearly 15 years on Mars and broke the driving record for putting the most miles on its odometer, ending its mission on Feb. 13, 2019. | planet.mars | apxs.mer1; apxs.mer2; descam.mer1; descam.mer2; hazcam.mer1; hazcam.mer2; imu.mer1; imu.mer2; mb.mer1; mb.mer2; mi.mer1; mi.mer2; mini-tes.mer1; mini-tes.mer2; navcam.mer1; navcam.mer2; pancam.mer1; pancam.mer2; rat.mer1; rat.mer2; rss.mer1; rss.mer2 | spacecraft.mer1; spacecraft.mer2 | 1 | 22 | 2 |
urn:nasa:pds:context:investigation:mission.mars_global_surveyor | mars_global_surveyor | Mars Global Surveyor | Mission | 1994-10-12T00:00:00 | 2006-11-14T00:00:00 | Mars Global Surveyor was an orbiting spacecraft that looped around the Red Planet for a decade. The mission overhauled scientists' understanding of Mars by studying the entire Martian surface, atmosphere, and interior. Major findings included dramatic evidence that water still flows on Mars in short bursts down hillside gullies, and the identification of water-related mineral deposits leading to selection of a Mars rover landing site for a subsequent mission. The mission continued sending images and other data until November 2006, when it went silent due to a series of events linked to a computer error likely caused by battery failure. | planet.mars; satellite.mars.phobos; star.sun | mgs.accel; mgs.er; mgs.mag; mgs.moc; mgs.mola; mgs.rss; mgs.tes | spacecraft.mgs | 3 | 7 | 1 |
urn:nasa:pds:context:investigation:mission.mars_observer | mars_observer | Mars Observer | Mission | 1992-09-25T00:00:00 | 1993-08-21T00:00:00 | Mars Observer was launched on September 25, 1992, from Cape Canaveral using a Titan III rocket. However, on August 21, 1993, contact was lost during the pre-Mars-Orbit-Insertion sequence, and efforts to re-establish communication failed. The spacecraft was intended to enter an elliptical orbit around Mars, subsequently adjusting to a near-circular, low altitude, sun-synchronous orbit for global mapping over a Martian year. The mission planned for continuous data collection and playback, with specific orbit trim adjustments for uniform coverage. Mars Observer featured a stabilized platform for its scientific instruments, including a Gamma Ray Spectrometer and Magnetometer. However, it lacked a movable scanning platform, relying instead on internal scanning mechanisms for its observations. | planet.mars | mo.rss | spacecraft.mo | 1 | 1 | 1 |
urn:nasa:pds:context:investigation:mission.2001_mars_odyssey | 2001_mars_odyssey | Mars Odyssey | Mission | 2001-01-04T00:00:00 | null | The 2001 Mars Odyssey mission consists of an orbiter that investigates the climate and geology of Mars. | planet.mars | ody.accel; ody.grs; ody.hend; ody.mar; ody.ns; ody.rss; ody.themis | spacecraft.ody | 1 | 7 | 1 |
urn:nasa:pds:context:investigation:mission.mars_pathfinder | mars_pathfinder | Mars Pathfinder | Mission | 1993-11-01T00:00:00 | 1998-03-10T00:00:00 | The Mars Pathfinder mission, designed to demonstrate a low-cost method for delivering a set of science instruments to the Red Planet, was the first wheeled vehicle to be used on any other planet in the solar system and served as the foundation for the Mars rovers of today. The mission landed a rover -- Sojourner -- on the surface of Mars using an air bag landing system and innovative petal design, which have been used since in various incarnations to land other rovers on the Red Planet. Sojourner spent 83 days of a planned seven-day mission exploring the Martian terrain, snapping photographs and taking chemical, atmospheric and other measurements | planet.mars; satellite.mars.deimos; satellite.mars.phobos; star.sun | asimet.mpfl; imp.mpfl; mpfr.apxs; mpfr.rclt; mpfr.rcrr; mpfr.rcrt; rss.mpfl; windsock.mpfl | spacecraft.mpfl; spacecraft.mpfr | 4 | 8 | 2 |
urn:nasa:pds:context:investigation:mission.phoenix | phoenix | Mars Phoenix | Mission | 2007-08-04T00:00:00 | 2008-11-02T00:00:00 | The Phoenix Mission was the first Scout class mission. It consisted of a single lander with associated instrumentation. Phoenix was launched on August 4, 2007 and landed on the northern plains of Mars (68.22 degrees N, 234.25 degrees East Areocentric) on May 25, 2008. The Lander operated until November 2, 2008, performing on the Martian surface for 152 sols (sols are Martian days, 1 sol equaling 24.66 hours). The Surface Phase constituted the primary and extended missions, and focused on testing the hypothesis that water ice exists beneath a thin soil cover, evaluating evidence for habitability zones, and monitoring weather during the northern summer. Hence, inferring the presence of water and its interaction with the Martian soil was of crucial importance. | planet.mars | ase.phx; lidar.phx; meca_afm.phx; meca_elec.phx; meca_tecp.phx; meca_wcl.phx; met.phx; om.phx; ra.phx; rac.phx; ssi.phx; tega.phx; tt.phx | spacecraft.phx | 1 | 13 | 1 |
urn:nasa:pds:context:investigation:mission.mars_reconnaissance_orbiter | mars_reconnaissance_orbiter | Mars Reconnaissance Orbiter | Mission | 2005-08-12T00:00:00 | null | The Mars Reconnaissance Orbiter, or MRO, has studied the Red Planet's atmosphere and terrain from orbit since 2006 and also serves as a key data relay station for other Mars missions, including the Mars Exploration Rover Opportunity. Equipped with a powerful camera called HiRISE that has aided in a number of discoveries, the Mars Reconnaissance Orbiter has sent back thousands of stunning images of the Martian surface that are helping scientists learn more about Mars, including the history of water flows on or near the planet's surface. | planet.mars | accel.mro; crism.mro; ctx.mro; hirise.mro; marci.mro; mcs.mro; rss.mro; sharad.mro | spacecraft.mro | 1 | 8 | 1 |
urn:nasa:pds:context:investigation:mission.mars_science_laboratory | mars_science_laboratory | Mars Science Laboratory: Curiosity Rover | Mission | 2003-10-01T00:00:00 | null | The Mars Science Laboratory (MSL) project, initiated in 2003, marked a significant advancement in Mars exploration with the successful deployment of the Curiosity rover. Launched on November 26, 2011, and landing in Gale Crater on August 6, 2012, the MSL mission has broadened our understanding of Martian environments and their potential habitability. Throughout its journey to Mars, and during its primary mission which concluded on September 28, 2014, Curiosity undertook comprehensive scientific investigations. These included routine instrument health checks and data collection by the Radiation Assessment Detector (RAD) during transit. On the Martian surface, Curiosity's primary objectives were to assess the biological potential of the landing site, characterize the landing region's geology, study planetary processes relevant to habitability, and quantify the spectrum of surface radiation. The rover gathered crucial data through imaging, spectroscopy, and other analytic techniques to evaluate the composition of Martian soils, rocks, and the atmosphere. These efforts have provided vital insights into Mars' habitability and environmental history. The continuation of these scientific objectives into Curiosity’s first extended mission aims to deepen the exploration of potentially habitable environments that could also preserve organic compounds. Additionally, the mission focuses on exploring and characterizing significant geological transitions in the region surrounding the foothills of Mt. Sharp. This ongoing research is pivotal for understanding the past and present potential for life on Mars and informs future exploratory missions to the Red Planet. | planet.mars | accel.msl; apxs.msl; chemcam_libs.msl; chemcam_rmi.msl; chemcam_soh.msl; chemin.msl; dan.msl; fhaz_left_a.msl; fhaz_left_b.msl; fhaz_right_a.msl; fhaz_right_b.msl; hazcam.msl; mahli.msl; mardi.msl; mast_left.msl; mast_right.msl; nav_left_a.msl; nav_left_b.msl; nav_right_a.msl; nav_right_b.msl; navcam.msl; rad.msl; rems.msl; rhaz_left_a.msl; rhaz_left_b.msl; rhaz_right_a.msl; rhaz_right_b.msl; sam.msl | spacecraft.msl | 1 | 28 | 1 |
urn:nasa:pds:context:investigation:mission.messenger | messenger | MErcury Surface, Space ENvironment, GEochemistry, and Ranging | Mission | 2004-08-03T00:00:00 | 2015-04-30T00:00:00 | Mercury Surface, Space Environment, Geochemistry, and Ranging (MESSENGER) launched in August 2004. It entered into orbit around Mercury on March 18, 2011. It was to study the chemical composition, geology, and magnetic field of Mercury. It impacted the planet on April 30, 2015. | calibrator.calibration; planet.earth; planet.mercury; planet.venus | epps-eps.mess; epps-fips.mess; grs.mess; mag.mess; mascs.mess; mdis-nac.mess; mdis-wac.mess; mla.mess; ns.mess; rss.mess; xrs.mess | spacecraft.mess | 4 | 11 | 1 |
urn:nasa:pds:context:investigation:mission.new_horizons_kem2 | new_horizons_kem2 | New Horizons Kuiper Belt Extended Mission 2 (KEM2) | Mission | 2022-10-01T00:00:00 | 2024-09-30T00:00:00 | The New Horizons Kuiper Belt Extended Mission (KEM) is a mission to a recently discovered, unexplored region of the solar system, the Kuiper Belt. The first part (KEM1) included a close flyby of Kuiper Belt Object (KBO) 2014 MU69 (Arrokoth). This second part (KEM2) continued to survey the Kuiper Belt using New Horizons as an observatory, examining many other Kuiper Belt Objects and Centaurs while studying the Kuiper Belt dust, gas, plasma, and energetic particle environments. These studies will place both the Pluto system and Arrokoth in better context among KBOs, increasing scientific understanding of both. New science goals for KEM2 include: new studies in Planetary Science (large-phase angle observations of gas giants), Heliophysics (Lyman-alpha all sky map), and Astrophysics (cosmic optical and ultraviolet background, and distant shock regions). KEM2 data deliveries also include data taken during KEM1 but not downlinked until KEM2. | dust.dust; plasma_stream.solar_wind; trans-neptunian_object.486958_2014_mu69 | nh.alice; nh.leisa; nh.lorri; nh.mvic; nh.pepssi; nh.rex; nh.sdc; nh.swap | spacecraft.nh | 3 | 8 | 1 |
urn:nasa:pds:context:investigation:individual.none | none | No Specific Investigation | Individual Investigation | null | null | This context object indicates there is no specific funded investigation associated with the product. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:observing_campaign.irtf_io | irtf_io | Observing Campaign for Io at NASA's InfraRed Telescope Facility (IRTF) | Observing Campaign | 1983-02-09T00:00:00 | null | Initially started as part of the PDART 2016 efforts of Dr. Ashley Davies to archive important Io observations from publications. This observing campaign can be used for past and future observations conducted at the IRTF for Io, the satellite of Jupiter. | satellite.jupiter.io | null | null | 1 | 0 | 0 |
urn:nasa:pds:context:investigation:observing_campaign.jupiter_support | jupiter_support | Observing Campaign for Support Monitoring of Jupiter | Observing Campaign | 2003-01-01T00:00:00 | null | Initially started as part of the PDART 2016 efforts of Dr. Glenn Orton to archive ground-based observations as part of an ongoing observing campaign to monitor Jupiter in support of past, present, and future missions to Jupiter. Any ground-based observations of Jupiter for this purpose should use this context reference. | planet.jupiter | null | null | 1 | 0 | 0 |
urn:nasa:pds:context:investigation:mission.pioneer_10 | pioneer_10 | Pioneer 10 | Mission | 1972-03-02T00:00:00 | 1997-03-31T00:00:00 | Pioneer 10 was the first spacecraft that went to Jupiter. It was also the first spacecraft to achieve escape velocity. It was launched on March 2, 1972. It was at 80 AU from Earth when it lost contact. | planet.jupiter; planetary_system.solar_system; plasma_stream.solar_wind | cpi.p10; crt.p10; go.epd; go.gdds; go.hic; go.mag; go.nims; go.pls; go.ppr; go.pws; go.rss; go.ssd; go.ssi; go.uvs; gtt.p10; hvm.p10; ipp.p10; pa.p10; trd.p10; uv.p10 | spacecraft.go; spacecraft.p10 | 3 | 20 | 2 |
urn:nasa:pds:context:investigation:mission.pioneer_11 | pioneer_11 | Pioneer 11 | Mission | 1972-03-02T00:00:00 | 1995-09-30T00:00:00 | NASA's Pioneer 11, a sister spacecraft to Pioneer 10, was the first spacecraft to study Saturn up close. The mission ended in 1995 and Pioneer 11 is on a trajectory to take it out of the solar system. Pioneer 11 is one of five spacecraft on a trajectory that will take them out of our solar system. Pioneer 11 will pass near the star Lambda Aquila in almost four million years. Like Pioneer 10 and Voyager 1 and 2, Pioneer 11 carries a message from humanity to the cosmos. | planet.jupiter; planet.saturn; planetary_system.solar_system | cpi.p11; crs.p11; crt.p11; fgm.p11; gtt.p11; hvm.p11; pa.p11; trd.p11; uv.p11 | spacecraft.p11 | 3 | 9 | 1 |
urn:nasa:pds:context:investigation:mission.pioneer_8 | pioneer_8 | Pioneer 8 | Mission | 1967-12-13T00:00:00 | 1996-08-22T00:00:00 | The Pioneer 8, Pioneer C, was launched on December 13, 1967. It was part of group of spacecrafts to study space weather at various points between Earth and the Sun. The spacecraft was in a solar orbit of 1.1 AU. | null | cdd.p8 | spacecraft.p8 | 0 | 1 | 1 |
urn:nasa:pds:context:investigation:mission.pioneer_9 | pioneer_9 | Pioneer 9 | Mission | 1968-11-18T00:00:00 | 1983-05-19T00:00:00 | The Pioneer 9, Pioneer D, was launched on November 8, 1968. It was part of group of spacecrafts to study space weather at various points between Earth and the Sun. The spacecraft was in a solar orbit of 0.8 AU. | null | cdd.p9 | spacecraft.p9 | 0 | 1 | 1 |
urn:nasa:pds:context:investigation:mission.pioneer_venus | pioneer_venus | Pioneer Venus | Mission | 1978-05-20T00:00:00 | 1992-10-07T00:00:00 | The Pioneer Venus was launched on May 20, 1978. It had an orbiter and four probes that entered the atmosphere. One probe had even transmitted data from the surface. The bus that carried the orbiter and probes also had mass spectrometers to study the atmosphere. The orbiter lasted until August 1992. | planet.venus | pvmp.bus.bims; pvmp.bus.bnms; pvmp.lp.las; pvmp.lp.lcps; pvmp.lp.lgc; pvmp.lp.lir; pvmp.lp.lnms; pvmp.lp.lsfr; pvmp.sp-day.sas; pvmp.sp-day.snfr; pvmp.sp-night.sas; pvmp.sp-night.snfr; pvmp.sp-north.sas; pvmp.sp-north.snfr; pvo.oad; pvo.ocpp; pvo.oefd; pvo.oetp; pvo.ogbd; pvo.oims; pvo.oir; pvo.omag; pvo.onms; pvo.opa; pvo.orad; pvo.orpa; pvo.orse; pvo.ouvs | spacecraft.pvmp.bus; spacecraft.pvmp.lp; spacecraft.pvmp.sp-day; spacecraft.pvmp.sp-night; spacecraft.pvmp.sp-north; spacecraft.pvo | 1 | 28 | 6 |
urn:nasa:pds:context:investigation:other_investigation.wt_threshold | wt_threshold | Planetary Boundary Layer Wind Tunnel Particle Threshold | Other Investigation | 2018-05-16T00:00:00 | null | Initially started as part of the PDART 2014 efforts of Devon Burr, this investigation is designed to acculumate planetary boundary layer wind tunnel data for planetary analogs of Mars, Venus, Titan, and Earth (and potentially others) for the purpose of investigating particle entrainment threshold wind speed data. Particle entrainment threshold denotes the wind speed at which a particle of a given size and density will begin to move in the airflow. Historically Ronald Greeley and James D. Iversen setup a series of wind tunnels to run in various planetary analog environments to investigate basic parameters for planetary aeolian processes spanning 1970s-2010s. This work is carried on by numerous former students and colleagues expanding what is known about sand and dust movement by wind processes on multiple planetary bodies. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:mission.pre-magellan | pre-magellan | PRE-MAGELLAN | Mission | 1968-11-09T00:00:00 | 1988-07-27T00:00:00 | Mission Overview ============================ This entity is a collection of selected Earth-based radar data of Venus, the Moon, Mercury, and Mars, Pioneer Venus radar data, airborne radar images of Earth, and line of sight acceleration data derived from tracking the Pioneer Venus Orbiter and Viking Orbiter 2. Included are 12.6 centimeter wavelength Arecibo Venus radar images, 12.6 to 12.9 cm Goldstone Venus radar images and altimetry data, together with altimetry, brightness temperature, Fresnel reflectivity and rms slopes derived from the Pioneer Venus Radar Mapper. For the Moon, Haystack 3.8 centimeter radar images and Arecibo 12.6 and 70 centimeter radar images are included. Mars data include Goldstone altimetry data acquired between 1971 and 1982 and a raster data set containing radar units that model Goldstone and Arecibo backscatter observations. Mercury data consist of Goldstone altimetry files. The terrestrial data were acquired over the Pisgah lava flows and the Kelso dune field in the Mojave Desert, California, and consist of multiple frequency, multiple incidence angle views of the same regions. Data set documentation is provided, with references that allow the reader to reconstruct processing histories. The entire data set collection and documentation are available on a CD-ROM entitled Pre-Magellan Radar and Gravity Data. PDS4 note: awaiting LID references to facilities and telescopes - ARECIBO OBSERVATORY - GOLDSTONE SOLAR SYSTEM RADAR - HAYSTACK OBSERVATORY - NASA DC-8 AIRCRAFT | planet.earth; planet.mars; planet.mercury; planet.venus; satellite.earth.moon | irtm.vo2; mawd.vo2; pvmp.lp.las; pvo.orad; rss.vo2; visa.vo2; visb.vo2 | spacecraft.pvo; spacecraft.vo2 | 5 | 7 | 2 |
urn:nasa:pds:context:investigation:observing_campaign.pre-magellan | pre-magellan | Pre-Magellan Radar and Gravity Observations | Observing Campaign | 1968-11-09T00:00:00 | 1988-07-27T00:00:00 | This dataset contains 15 radar, altimetry, and gravity data sets, including extensive Earth-based radar observations of the Earth's Moon and the inner planets, spanning the years 1968-1990. These datasets were prepared in advance of the Magellan Mission to Venus (1990-1994) in order to provide a set of relevant radar and gravity data for comparison to Magellan data. | planet.earth; planet.mars; planet.mercury; planet.venus; satellite.earth.moon | arecibo.305m.recv_s; arecibo.305m.trans_s; goldstone.dss13_34m.recv_x; goldstone.dss14_70m.recv_x; goldstone.dss14_70m.trans_x; pvo.orad; pvo.orse; rss.vo2 | spacecraft.pvo; spacecraft.vo2 | 5 | 8 | 2 |
urn:nasa:pds:context:investigation:individual.greeley_field_amboycrater | greeley_field_amboycrater | R. Greeley Field Investigation, Amboy Crater, California | Individual Investigation | 1976-01-01T00:00:00 | 1976-01-01T00:00:00 | In 1976, Dr. Ronald Greeley and Dr. James Iversen used hand-held cameras to acquire photographs of the volcanic cindercone Amboy Crater and its surrounding lava flows, located in the Mojave Desert of southeast California. These photographs are mostly black and white (but some are color) and were taken at low altitude from a fixed-wing aircraft, on the ground near volcanic outcrops, and of flows from close up. The purpose of the images was to depict volcanic features on Earth that could be studied as an analog to features similar to those found on Mars and the Moon. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:other_investigation.relab_speclib | relab_speclib | RELAB Reflectance Spectra Measurements | Other Investigation | 1981-02-10T00:00:00 | 2017-06-18T00:00:00 | Spectroscopic data acquired in RELAB provide the interpretive foundation upon which compositional information about unexplored or unsampled planetary surfaces is derived from remotely obtained reflectance spectra. The Keck/NASA Reflectance Experiment Laboratory (RELAB, http://planetary.brown.edu/relab/) is supported by NASA as a multi-user spectroscopy facility, and laboratory time can be made available at no charge to investigators who are in funded NASA programs. RELAB has two operational spectrometers available to NASA scientists: 1) a near-ultraviolet, visible, and near-infrared bidirectional spectrometer and 2) a near- and mid- infrared FT-IR spectrometer. The overall purpose of the design and operation of the RELAB bidirectional spectrometer is to obtain high precision, high spectral resolution, bidirectional reflectance spectra of earth and planetary materials. One of the key elements of its design is the ability to measure samples using viewing geometries specified by the user. This allows investigators to simulate the geometry of natural observing conditions for particulate samples as small as 50 mg. | null | relab.bc-ftir1; relab.bcf-ftir2; relab.bd-vnir | null | 0 | 3 | 0 |
urn:nasa:pds:context:investigation:other_investigation.relab_speclib | relab_speclib | RELAB Spectral Library | Other Investigation | 1981-02-10T00:00:00 | null | The RELAB Spectral Library is a database of reflectance spectra collected by the NASA Relectance Experiment Laboratory, along with ancillary chemistry and image information. | null | relab.bc-ftir1; relab.bcf-ftir2; relab.bd-vnir | null | 0 | 3 | 0 |
urn:nasa:pds:context:investigation:observing_campaign.saturn_occultation_of_28_sagittarius_1989 | saturn_occultation_of_28_sagittarius_1989 | Saturn Occultation of 28 Sagittarius (1989) | Observing Campaign | 1989-07-03T00:00:00 | 1989-07-03T00:00:00 | On 3 July 1989 an occultation of the bright star 28 Sagittarii provided a rare opportunity for occultation observations of both Saturn and its rings with Earth-based telescopes. Prior to 1989, most of our quantitative knowledge of the optical depths and detailed radial structure in the Saturn ring system was derived from occultation experiments carried out by the Voyager spacecraft. The data acquired during this event provided important details on the state and evolution of Saturn's ring system during the period between Voyager and Cassini. | planet.saturn; ring.saturn.rings | multi-host.generic_insp_hsp | null | 2 | 1 | 0 |
urn:nasa:pds:context:investigation:observing_campaign.saturn_ring_plane_crossing_1995 | saturn_ring_plane_crossing_1995 | Saturn Ring Plane Crossing (1995) | Observing Campaign | 1994-01-01T00:00:00 | 1997-01-01T00:00:00 | The 1995-1996 Saturn Ring Plane Crossing (RPX) occurred as the Earth passed through the plane of Saturn's rings three times. During this period, astronomers were eager to carry out out a wide range of Saturn observations. The three crossings occurred on May 22, 1995; August 10, 1995; and February 11, 1996. Additionally, the Sun crossed the plane of Saturn’s rings on November 17-21, 1995. Saturn RPX events only occur every 13-15 years, and poor viewing geometry as seen from Earth characterizes the 2009 and 2025 events (though the 2009 event was spectacularly observed by the Cassini spacecraft from Saturn orbit). The next favorable Earth-based viewing of a Saturn RPX will be in 2038-2039. The period around a Saturn RPX enables Earth-based astronomers to study a wide range of phenomena not observable at any other time. Direct measurements of ring thickness and vertical ring warps become possible. Precise timing of the crossings makes it possible to better determine Saturn's rotation pole. With the rings becoming very thin and faint, detections of faint outer rings and tiny ring-moons become possible. Also, satellite eclipses, occultations and mutual events during the RPX period can be used to refine satellite orbits throughout the Saturn system. The data acquired during the 1995-1996 RPX events comprise some of the best obtained since the Voyager encounters with Saturn and serve as a useful bridge between the Voyager and Cassini observations of Saturn. | planet.saturn; satellite.saturn.atlas; satellite.saturn.calypso; satellite.saturn.dione; satellite.saturn.enceladus; satellite.saturn.epimetheus; satellite.saturn.helene; satellite.saturn.hyperion; satellite.saturn.iapetus; satellite.saturn.janus; satellite.saturn.mimas; satellite.saturn.pan; satellite.saturn.pandora; satellite.saturn.prometheus; satellite.saturn.rhea; satellite.saturn.telesto; satellite.saturn.tethys; satellite.saturn.titan | hst.acs; hst.cos; hst.fgs; hst.foc; hst.hsp; hst.hstacs; hst.nicmos; hst.stis; hst.wfc3; hst.wfpc2; rebelxt.n-a | spacecraft.hst | 18 | 11 | 1 |
urn:nasa:pds:context:investigation:observing_campaign.saturn_small_satellite_astrometry | saturn_small_satellite_astrometry | Saturn Small Satellite Astrometry | Observing Campaign | 1994-12-01T00:00:00 | 2005-01-14T00:00:00 | A long-term observing campaign of Saturn Small Satellite Astrometry was undertaken from 1994 to 2005 to extend the time line of astrometric observations of Prometheus and Pandora and other Saturnian moons in order to refine their ephemerides. This was done in response to the discovery, during the 1995-1996 Saturn Ring Plane Crossing (RPX) event, that the positions of Saturn’s moons Prometheus and Pandora varied significantly from the predictions of their positions based on Voyager observations. The goal was to determine the cause(s) of the discrepancies. This campaign used archival HST data from 1994, previously unexamined RPX images, and a large series of targeted WFPC2 observations between 1996 and 2005. Sufficient observations to produce astrometrically meaningful data for nine other satellites were obtained incidentally in the Prometheus-Pandora observing campaign. Details of the project can be found in French et al., 2006 | satellite.saturn.calypso; satellite.saturn.dione; satellite.saturn.enceladus; satellite.saturn.epimetheus; satellite.saturn.helene; satellite.saturn.hyperion; satellite.saturn.janus; satellite.saturn.mimas; satellite.saturn.pandora; satellite.saturn.prometheus; satellite.saturn.rhea; satellite.saturn.telesto; satellite.saturn.tethys; satellite.saturn.titan | hst.acs; hst.cos; hst.fgs; hst.foc; hst.hsp; hst.hstacs; hst.nicmos; hst.stis; hst.wfc3; hst.wfpc2 | spacecraft.hst | 14 | 10 | 1 |
urn:nasa:pds:context:investigation:individual.catalina_sky_survey | catalina_sky_survey | The Catalina Sky Survey (CSS) | Individual Investigation | 1998-01-01T00:00:00 | null | The Catalina Sky Survey (CSS) is a NASA funded, ground-based sky survey fully dedicated to the discovery and tracking of near-Earth objects (NEOs). | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:mission.contour_mission | contour_mission | The Comet Nucleus Tour (CONTOUR) Mission | Mission | 2002-07-05T00:00:00 | 2002-08-15T00:00:00 | The Comet Nucleus Tour mission failed when the spacecraft broke apart during a planned maneuver six weeks after launch. No data were returned. | null | con.cfi; con.cida; con.crispimag; con.crispspec; con.ngims | spacecraft.con | 0 | 5 | 1 |
urn:nasa:pds:context:investigation:mission.dawn_mission_to_vesta_and_ceres | dawn_mission_to_vesta_and_ceres | The Dawn Mission to Vesta and Ceres | Mission | 2007-09-27T00:00:00 | 2016-07-01T00:00:00 | The Dawn mission launched in Sept. 2007 to rendezvous and orbit the asteroid (4) Vesta and the dwarf planet (1) Ceres. Vesta orbit operations took place from July 2011 to Sept. 2012, and Ceres orbit operations from March 2015 to Oct. 2018. The scientific objectives of the mission were to characterize the asteroids' internal structure, density, shape, size, composition and mass and to return data on surface morphology, cratering, and magnetism. Communication with the spacecraft was lost after hydrazine exhaustion in October 2018. | asteroid.4_vesta; dwarf_planet.1_ceres; planet.mars | dawn.fc1; dawn.fc2; dawn.grand; dawn.rss; dawn.vir | spacecraft.dawn | 3 | 5 | 1 |
urn:nasa:pds:context:investigation:mission.deep_impact | deep_impact | The Deep Impact Mission | Mission | 2005-01-12T00:00:00 | 2005-07-13T00:00:00 | The Deep Impact mission consisted of an impactor and a fly-by spacecraft that rendezvoused with comet 9P/Tempel 1. The impactor was released to impact the comet surface on July 4 2005, while the flyby spacecraft observed. | calibrator.calibration; comet.9p_tempel_1 | dif.hrii; dif.hriv; dif.mri; dif.rss; dii.its | spacecraft.dif; spacecraft.dii | 2 | 5 | 2 |
urn:nasa:pds:context:investigation:mission.double_asteroid_redirection_test | double_asteroid_redirection_test | The Double Asteroid Redirection Test (DART) Mission | Mission | null | null | The DART mission was a planetary defense and technology demonstration mission that impacted the moon (Dimorphos) of the Didymos asteroid system to measure the effect on the moon's orbit. | asteroid.65803_didymos; satellite.65803_didymos.dimorphos | dart.draco; dart.hga; liciacube.hga; liciacube.leia; liciacube.luke | spacecraft.dart; spacecraft.liciacube | 2 | 5 | 2 |
urn:nasa:pds:context:investigation:mission.epoxi | epoxi | The EPOXI Joint Missions | Mission | 2007-09-26T00:00:00 | 2013-09-20T00:00:00 | "EPOXI" is the moniket assigned to the two extended missions for the Deep Impact spacecraft: the Extrasolar Planet Observation and Characterization (EPOCh) Mission, and the Deep Impact Extended Investigation (DIXI) mission. As part of the DIXI mission, the spacecraft flew by Comet 103P/Hartley 2. As part of the EPOCh mission, the spacecraft used the larger of its two telescopes to find extrasolar planets using the transit method. | calibrator.calibration; comet.103p_hartley_2; comet.c2009_p1_garradd; comet.c2012_s1_ison; planet.earth; planet.mars; star.1swasp_j175207.01_373246.3; star.bd_36_2593; star.bd_47_2846; star.kepler-1; star.moa_2009-blg-266; star.ross_905; star.wasp-3; star.xo-2; star.xo-3 | dif.hrii; dif.hriv; dif.mri; dif.rss | spacecraft.dif | 15 | 4 | 1 |
urn:nasa:pds:context:investigation:mission.hayabusa | hayabusa | The Hayabusa Mission | Mission | 2003-05-09T00:00:00 | 2010-06-13T00:00:00 | The Hayabusa (formerly MUSES-C) mission was a JAXA mission that successfully encountered and collected sampled from asteroid (25143) Itokawa in September-November 2005, returning those samples to Earth. The spacecraft itself burned up on reentry into Earth's atmosphere, as planned. | asteroid.25143_itokawa | amica.hay; lidar.hay; nirs.hay | spacecraft.hay | 1 | 3 | 1 |
urn:nasa:pds:context:investigation:mission.infrared_astronomical_satellite | infrared_astronomical_satellite | The Infrared Astronomical Satellite (IRAS) Mission | Mission | 1983-01-26T00:00:00 | 1983-11-23T00:00:00 | The IRAS mission was a joint program of the USA, the Netherlands, and the UK to conduct a survey of the sky in four IR wavelengths. It also made pointed observatons of selected astronomical and solar system objects. | null | iras.fpa | spacecraft.iras | 0 | 1 | 1 |
urn:nasa:pds:context:investigation:mission.international_cometary_explorer | international_cometary_explorer | The International Sun-Earth Explorer-3/International Cometary Explorer | Mission | 1983-12-22T00:00:00 | null | The International Cometary Explorer (ICE) became part of the Halley Armada to study comet Halley in 1986. It was first place in the Earth-Sun L1 position under the name of International Sun/Earth Explorer 3 (ISEE-3). It was to study the Sun-Earth relationship beyond the Earth's magnetosphere. As the part of the armada, it went through the tail of Halley to collect data. In 2014, a crowdfunding group tried to use it for another comet pass, but it lost contact with the spacecraft. | comet.21p_giacobini-zinner | ice.epas; ice.ici; ice.mag; ice.plawav; ice.radwav; ice.swp; ice.uleca | spacecraft.ice | 1 | 7 | 1 |
urn:nasa:pds:context:investigation:mission.light_italian_cubesat_for_imaging_of_asteroids | light_italian_cubesat_for_imaging_of_asteroids | The Light Italian CubeSat for Imaging of Asteroids (LICIACube) Mission | Mission | 2021-11-24T00:00:00 | null | The LICIACube mission was a mission of the Agenzia Spaziale Italiana (ASI) that was carried by the Double Asteroid Redirection Test (DART) mission impactor spacecraft to the vicinity of the Didymos system. It was then released 15 days before the DART impact into Dimorphos to observe the impact and aftermath of the collision of DART with Dimorphos. | asteroid.65803_didymos; satellite.65803_didymos.dimorphos | liciacube.hga; liciacube.leia; liciacube.luke | spacecraft.liciacube | 2 | 3 | 1 |
urn:nasa:pds:context:investigation:individual.lowell_observatory_near_earth_object_survey | lowell_observatory_near_earth_object_survey | The Lowell Observatory Near-Earth Object Survey (LONEOS) | Individual Investigation | 1998-01-01T00:00:00 | 2008-01-01T00:00:00 | The LONEOS was a 10-year, ground-based program at Lowell Observatory to search for Near Earth Objects. It consisted of two parts, LONEOS-1 spanning 1993-2000, and LONEOS-2, conducted with a more sensitive camera, spanning 2000-2008. | null | null | null | 0 | 0 | 0 |
urn:nasa:pds:context:investigation:mission.lucy | lucy | The Lucy Mission | Mission | 2021-10-16T00:00:00 | null | Lucy will be the first space mission to explore a population of small bodies known as the JupiterTrojan asteroids. This mission plan includes encounters with three main belt alsteroid and eight Jupiter Trojans. The Lucy spacecraft also observed the impact of the DART spacecraft into the Dimorphos, the moon of the Didymos system. | asteroid.11351_leucus; asteroid.15094_polymele; asteroid.152830_dinkinesh; asteroid.21900_orus; asteroid.3548_eurybates; asteroid.52246_donaldjohanson; asteroid.617_patroclus; satellite.617_patroclus.menoetius | lucy.leisa; lucy.llorri; lucy.ltes; lucy.mvic; lucy.prop; lucy.rss; lucy.ttcam | spacecraft.lucy | 8 | 7 | 1 |
urn:nasa:pds:context:investigation:mission.mariner71 | mariner71 | The Mariner Mars '71 (Mariner 9) Mission | Mission | 1968-06-01T00:00:00 | 1973-06-01T00:00:00 | On November 14, 1971, Mariner 9 became the first spacecraft to orbit another planet when it established orbit around Mars. Six experiments were carried as part of the science payload: television, ultraviolet spectrometer, infrared spectroscopy, infrared radiometry, S-band occultation and celestial mechanics. The mission was originally planned as a pair, similar to the Mariner 6 and 7 missions, but Mariner 8 was lost because of guidance difficulties in the second stage of the launch vehicle. It was determined that an orbit for a single-spacecraft mission could be developed to meet all basic mission and specific science objectives. A single-spacecraft plan, involving an inclination of 65 degrees, a period of about 12 hours, a periapsis altitude of 1350 Km, and an arrival date of November 14, 1971, was evaluated and formalized in 2 weeks. Mariner 9 carried on the Mariner program investigation of the Martian atmosphere, and mapping of the Martian surface at the highest resolution yet achieved at the time. | planet.mars | iris.mr9; iss.mr9; rss.mr9; uvs.mr9 | spacecraft.mr9 | 1 | 4 | 1 |
urn:nasa:pds:context:investigation:mission.midcourse_space_experiment | midcourse_space_experiment | The Midcourse Space Experiment | Mission | 1996-04-24T00:00:00 | 1997-02-26T00:00:00 | The Midcourse Space Experiment (MSX) was launched in 1996 by the U.S. Ballistic Missile Defence Organization (renamed the "Missile Defense Agency" in 2002) as a technology demonstration mission. Part of its mission included mapping the galactic plane in the Infrared, imaging the moon, and surveying small bodies. | dust.dust; satellite.earth.moon | msx.spirit3 | spacecraft.msx | 2 | 1 | 1 |
urn:nasa:pds:context:investigation:mission.near_earth_asteroid_rendezvous | near_earth_asteroid_rendezvous | The Near Earth Asteroid Rendezvous (NEAR) Mission | Mission | 1996-02-17T00:00:00 | 2001-02-28T00:00:00 | The Near Earth Asteroid Rendezvous (NEAR) mission to the near-earth asteroid 433 Eros was launched in Feb. 1996 and carried out Eros orbital operations from Feb. 2000 through Feb. 2001. It acquired the first comprehensive, spatially resolved measurements of the geomorphology, reflectance spectral properties, and shape of an asteroid, and X-ray and gamma-ray spectral measurements of elemental abundances from orbit and the surface. The ambient magnetic field in the vicinity of Eros was also measured. On the way to Eros, the spacecraft also performed a flyby of the asteroid 253 Mathilde in June 1997, obtaining image data and a mass determination. | asteroid.253_mathilde; asteroid.433_eros; comet.c1996_b2_hyakutake; magnetic_field.interplanetary_magnetic_field; planet.earth; planetary_system.solar_system; satellite.earth.moon | grs.near; mag.near; msi.near; nis.near; nlr.near; rss.near; xrs.near | spacecraft.near | 7 | 7 | 1 |
urn:nasa:pds:context:investigation:mission.neas | neas | The Near Earth Asteroid Scout (NEAS) Mission | Mission | 2021-11-23T00:00:00 | null | The NEAS mission was intended as a technology test/demonstration for developing a CubetSat with a solar sail that could be deployed to Near-Earth Asteroids (NEA). It was one of 10 CubeSats launched on Artemis 1 on 16 November 2022. The mission was lost when no communication could be established with the CubeSat post-launch. | asteroid.16_psyche | neas.neacam | spacecraft.neas | 1 | 1 | 1 |
urn:nasa:pds:context:investigation:individual.near_earth_asteroid_tracking | near_earth_asteroid_tracking | The Near-Earth Asteroid Tracking (NEAT) Survey | Individual Investigation | 1996-04-17T00:00:00 | 2007-04-15T00:00:00 | The NEAT survey discovered and tracked near-Earth asteroids and comets using telescopes in Hawai'i and at Palomar Observatory over the period December 1995 - April 2007. | null | null | null | 0 | 0 | 0 |
NASA PDS Planetary Missions Catalog
Part of the Space Probes & Mission Datasets collection on Hugging Face.
Comprehensive catalog of 137 planetary science investigations (missions), 115 instrument hosts (spacecraft), and 748 scientific instruments from the NASA Planetary Data System (PDS). Includes mission dates, target bodies, and full cross-references between missions, spacecraft, and instruments.
Dataset description
The NASA Planetary Data System is the official archive for all NASA planetary science data. Its context catalog defines every mission, spacecraft, and instrument that has contributed data to the archive. This dataset extracts those three entity types into linked tables, making it easy to explore the full landscape of planetary exploration — from Pioneer and Voyager through Perseverance and Psyche.
Each entity includes its PDS Logical Identifier (LID), which serves as a stable cross-reference key. Target bodies, instruments, and spacecraft are linked via semicolon-separated reference columns that can be split and joined across the three configs.
Configs
This dataset has three configs (tables):
missions (137 rows)
Planetary science investigations including orbital missions, flybys, landers, rovers, field campaigns, and observing programs.
| Column | Type | Description |
|---|---|---|
lid |
string | PDS Logical Identifier (unique key) |
short_name |
string | Short machine-friendly name extracted from LID |
name |
string | Full mission/investigation name |
type |
string | Investigation type (Mission, Field Campaign, etc.) |
start_date |
datetime | Mission start date (UTC) |
stop_date |
datetime | Mission stop date (UTC) |
description |
string | Free-text description of the investigation |
target_refs |
string | Semicolon-separated target body identifiers |
instrument_refs |
string | Semicolon-separated instrument identifiers |
spacecraft_refs |
string | Semicolon-separated spacecraft identifiers |
num_targets |
int32 | Number of target bodies |
num_instruments |
int32 | Number of instruments |
num_spacecraft |
int32 | Number of spacecraft |
spacecraft (115 rows)
Instrument hosts: spacecraft, landers, rovers, ground stations, telescopes, and other platforms.
| Column | Type | Description |
|---|---|---|
lid |
string | PDS Logical Identifier (unique key) |
short_name |
string | Short machine-friendly name extracted from LID |
name |
string | Full spacecraft/host name |
type |
string | Host type (Spacecraft, Rover, Lander, etc.) |
description |
string | Free-text description |
investigation_refs |
string | Semicolon-separated mission identifiers |
instrument_refs |
string | Semicolon-separated instrument identifiers |
target_refs |
string | Semicolon-separated target body identifiers |
num_investigations |
int32 | Number of linked missions |
num_instruments |
int32 | Number of instruments on this host |
num_targets |
int32 | Number of target bodies |
instruments (748 rows)
Scientific instruments across all missions and platforms.
| Column | Type | Description |
|---|---|---|
lid |
string | PDS Logical Identifier (unique key) |
name |
string | Full instrument name |
type |
string | Instrument type (Imager, Spectrometer, etc.) |
host_short_name |
string | Short name of host spacecraft (from LID) |
description |
string | Free-text description |
investigation_refs |
string | Semicolon-separated mission identifiers |
num_investigations |
int32 | Number of linked missions |
Quick stats
- 137 investigations: Mission (98), Individual Investigation (19), Observing Campaign (10), Other Investigation (8), Field Campaign (2)
- 115 instrument hosts: Spacecraft (108), Lander (6), Rover (1)
- 748 instruments: null (743), Spectrometer (3), Imager (1), Radio-Radar (1)
Usage
from datasets import load_dataset
# Load all three configs
missions = load_dataset("juliensimon/pds-planetary-missions", "missions", split="train").to_pandas()
spacecraft = load_dataset("juliensimon/pds-planetary-missions", "spacecraft", split="train").to_pandas()
instruments = load_dataset("juliensimon/pds-planetary-missions", "instruments", split="train").to_pandas()
# All missions targeting Mars
mars = missions[missions["target_refs"].str.contains("mars", case=False, na=False)]
print(mars[["name", "type", "start_date"]].to_string())
# Instruments on the Cassini spacecraft
cassini_inst = instruments[instruments["host_short_name"] == "co"]
print(cassini_inst[["name", "type"]].to_string())
# Spacecraft with the most instruments
spacecraft.nlargest(10, "num_instruments")[["name", "type", "num_instruments"]]
# Cross-reference: find all instruments for a mission
mission_lid = missions.loc[missions["name"].str.contains("Galileo", case=False), "instrument_refs"].iloc[0]
if mission_lid:
inst_lids = [f"urn:nasa:pds:context:instrument:{ref}" for ref in mission_lid.split("; ")]
galileo_instruments = instruments[instruments["lid"].isin(inst_lids)]
Data source
NASA Planetary Data System (PDS) Search API — the official NASA archive for planetary science data. The context catalog is maintained by PDS discipline nodes and updated as new missions and instruments are registered.
Related datasets
- deep-space-probes — Detailed deep space probe catalog from GCAT
- cassini-saturn-observations — Cassini mission observation log
- esa-mars-express-observations — ESA Mars Express observation log
- nasa-eva-chronology — NASA EVA history
Pipeline
Source code: juliensimon/space-datasets
Support
If you find this dataset useful, please give it a ❤️ on the dataset page and share feedback in the Community tab! Also consider giving a ⭐️ to the space-datasets repo.
Citation
@dataset{pds_planetary_missions,
author = {Simon, Julien},
title = {NASA PDS Planetary Missions Catalog},
year = {2026},
publisher = {Hugging Face},
url = {https://huggingface.co/datasets/juliensimon/pds-planetary-missions},
note = {Based on NASA Planetary Data System (PDS) context catalog via the PDS Search API}
}
License
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