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int32
UNIQUE_STORY_INDEX
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7,072
7072
196
5
0
Meanwhile, training of the first groups of Iranian crews by the U.S. Navy was underway in the US; one of these conducted a successful shoot-down with a Phoenix missile of a target drone flying at 50000 feet .
50,000
7,073
7073
140
5
0
The TF30 had been plagued from the start with susceptibility to compressor stalls at high AoA and during rapid throttle transients or above 30000 feet .
30,000
7,075
7075
68
5
0
Another benefit was allowing the Tomcat to cruise comfortably above 30000 feet , which increased its range and survivability.
30,000
7,076
7076
20
5
0
hardpoint capacity= 14500 pounds of ordnance and fuel tanks Baugher, Joe. [
14,500
7,078
7078
42
4
0
The F-117A's split internal bay can carry 5000 pounds of ordnance.
5,000
7,079
7079
45
5
0
The F-117 has a radar cross-section of about 0.001 meters square .
0
7,080
7080
84
4
0
The aircraft would be optionally fitted with hardpoints, allowing for an additional 8000 pounds of payload, and a new ground-attack radar with air-to-air capability.
8,000
7,081
7081
117
2
0
For the single-engined fighter the Navy requested the maximum obtainable speed, and a stalling speed not higher than 70 mph .
70
7,082
7082
192
4
0
After mock-up inspection in February 1939, construction of the XF4U-1 powered by an XR-2800-4 prototype of the Pratt & Whitney R-2800 Double Wasp twin-row, 18-cylinder radial engine, rated at 1805 horsepower went ahead quickly, as the very first airframe ever designed from the start to have a Double Wasp engine fitted ...
1,805
7,083
7083
134
3
0
On 1 October 1940, the XF4U-1 became the first single-engine U.S. fighter to fly faster than by flying at an average ground speed of 405 mph from Stratford to Hartford.
405
7,084
7084
42
3
0
In full-power dive tests, speeds of up to 550 mph were achieved, but not without damage to the control surfaces and access panels and, in one case, an engine failure.
550
7,085
7085
1
4
0
2000 horsepower Pratt & Whitney R-2800-8 in a Goodyear FG-1 Corsair
2,000
7,086
7086
67
4
0
The F4U incorporated the largest engine available at the time, the 2000 horsepower 18-cylinder Pratt & Whitney R-2800 Double Wasp radial.
2,000
7,087
7087
111
2
0
To extract as much power as possible, a relatively large Hamilton Standard Hydromatic three-blade propeller of 13 feet was used.
13
7,088
7088
92
1
0
These potentially lethal characteristics were later solved through the addition of a small, 6 inches -long stall strip to the leading edge of the outer right wing, just outboard of the gun ports.
6
7,089
7089
216
2
0
https://www.militaryfactory.com/aircraft/detail.asp?aircraft_id=87#armament 12] 12 Accordingly, as a 237 gal (897 l) self-sealing fuel tank replaced the fuselage mounted armament, the cockpit had to be moved back by 32 inches and the fuselage lengthened.
32
7,090
7090
63
1
0
In addition, 150 lb of armor plate was installed, along with a 1 inches bullet-proof windscreen which was set internally, behind the curved Plexiglas windscreen.
1
7,091
7091
72
2
0
The F4U-1 was considerably faster than the Grumman F6F Hellcat and only 13 mph slower than the Republic P-47 Thunderbolt; Hanson, Dave. [
13
7,092
7092
49
5
0
But while the P-47 achieved its highest speed at 30020 feet with the help of an intercooled turbocharger, Dean 1997, p. 281.
30,020
7,093
7093
39
5
0
the F4U-1 reached its maximum speed at 19900 feet , Tillman 1979, p. 196.
19,900
7,096
7096
153
1
0
In Royal Navy service, because of the limited hangar deck height in several classes of British carrier, many Corsairs had their outer wings "clipped" by 8 inches to clear the deckhead.
8
7,097
7097
89
1
0
Among these were a bulged canopy (similar to the Malcolm Hood), raising the pilot's seat 7 inches , Goebel, Greg. [
7
7,098
7098
181
4
0
Royal Canadian Navy Volunteer Reserve pilot, Lieutenant Robert Hampton Gray, of 1841 Squadron was hit by flak but pressed home his attack on a Japanese destroyer, sinking it with a 1000 pounds bomb but crashing into the sea.
1,000
7,099
7099
57
1
0
These were clipped-wing Corsairs, the wingtips shortened 8 inches to clear the lower overhead height of RN carriers.
8
7,100
7100
30
2
0
The cockpit was moved back by 32 inches .
32
7,101
7101
31
3
0
The fuselage was lengthened by 1.0 feet .
1
7,103
7103
36
1
0
2, p. 2 The pilot's seat was raised 7 inches which, combined with the new canopy and a 6-inch (152.4 mm) lengthening of the tailwheel strut, allowed the pilot better visibility over the long nose.
7
7,104
7104
28
1
0
These Corsairs introduced a 6 inches -long stall strip just outboard of the gun ports on the right wing leading edge and improved undercarriage oleo struts which eliminated bouncing on landing, making these the first truly "carrier capable" F4Us.
6
7,105
7105
62
1
0
In British service, they were modified with "clipped" wings ( 8 inches was cut off each wingtip) for use on British aircraft carriers, although the Royal Navy had been successfully operating the Corsair Mk I since 1 June 1943 when No.
8
7,106
7106
75
4
0
With drop tanks fitted, the fighter had a maximum ferry range of just over 1500 miles .
1,500
7,107
7107
36
3
0
This change gave the aircraft up to 250 horsepower more power, which, in turn, increased performance.
250
7,109
7109
11
4
0
It had the 2100 horsepower dual-stage-supercharged -18W engine.
2,100
7,110
7110
86
4
0
When the cylinders were injected with the water/alcohol mixture, power was boosted to 2450 horsepower .
2,450
7,111
7111
31
3
0
Maximum speed was increased to 448 mph and climb rate to over 4,500 ft/min (1,180 m/min) as opposed to the 2,900 ft/min (884 m/min) of the F4U-1A. US Navy performance trials The "4-Hog" retained the original armament and had all the external load (i.e., drop tanks, bombs) capabilities of the F4U-1D. The windscreen was ...
448
7,112
7112
63
2
0
F4U-4B: 300 F4U-4s ordered with alternate gun armament of four 20 mm AN/M3 cannon.
20
7,113
7113
22
4
0
rated at a maximum of 2760 horsepower .
2,760
7,114
7114
18
3
0
Maximum speed was 408 knots and max rate of climb at sea level 4,850 feet per minute.
408
7,116
7116
304
6
0
Durability, service life, and special requirements for some type of cells Stationary fuel cell applications typically require more than 40,000 hours of reliable operation at a temperature of −35 °C to 40 °C (−31 °F to 104 °F), while automotive fuel cells require a 5,000-hour lifespan (the equivalent of 150000 miles ) u...
150,000
7,117
7117
74
3
0
Molten carbonate fuel cells (MCFCs) require a high operating temperature, 650 °C , similar to SOFCs.
650
7,119
7119
115
7
0
TÜV SÜD Industrie Service GmbH, accessed on 2 August 2011 As of June 2011 demonstration FCEVs had driven more than 3000000 miles , with more than 27,000 refuelings.
3,000,000
7,120
7120
116
5
0
DOE Fuel Cell Technologies Program, FY 2010 Annual Progress Report, accessed 2 August 2011 and a durability of over 75000 miles with less than 10% degradation. [
75,000
7,121
7121
31
6
0
UTC buses had driven more than 600000 miles by 2011. [
600,000
7,123
7123
47
2
0
The flight lasted 10 minutes at an altitude of 80 meters , although the fuel cell reportedly had enough fuel to fly for two hours.
80
7,125
7125
73
2
0
The pellets are physically robust and operate at temperatures as warm as 50 Coulomb .
50
7,126
7126
87
3
0
In 1951 or 1952 he proposed the MOUSE ("Minimal Orbital Unmanned Satellite, Earth"), a 100 pounds satellite that would contain Geiger counters for measuring cosmic rays, photo cells for scanning the Earth, telemetry electronics for sending data back to Earth, a magnetic data storage device, and rudimentary solar energy...
100
7,127
7127
30
2
0
The rockets weighed less than 25 pounds and could be built for around $2000.
25
7,128
7128
65
5
0
Fired from a converted Navy LSM, they could reach an altitude of 50000 feet and had a complete telemetry system to send back information on cosmic, ultraviolet and X-rays.
50,000
7,129
7129
171
5
0
In a January 1960 presentation to the American Physical Society, Singer sketched out his vision of what the environment around the earth might consist of, extending up to 40000 miles into space.
40,000
7,132
7132
36
4
0
Singer argued that it would rise to 3000 feet then be rained out after a few days. "
3,000
7,133
7133
1
1
0
8 cms
8
7,134
7134
1
1
0
6 cms
6
7,135
7135
1
1
0
6 cms
6
7,136
7136
1
1
0
6 cms http://www.fishbase.org/Summary/SpeciesSummary.php?ID=12199&AT=Threestripe+corydoras Fishbase:thilineatus
6
7,137
7137
1
2
0
16 cms
16
7,138
7138
1
2
0
50 cms
50
7,139
7139
1
3
0
120 cms
120
7,141
7141
1
2
0
30 cms
30
7,142
7142
1
3
0
104 cms
104
7,143
7143
1
3
0
130 cms
130
7,144
7144
1
3
0
178 cms
178
7,146
7146
1
2
0
90 cms
90
7,147
7147
1
1
0
9 cms
9
7,148
7148
1
2
0
71 cms
71
7,149
7149
1
3
0
130 cms
130
7,150
7150
1
2
0
50 cms
50
7,151
7151
1
3
0
130 cms
130
7,152
7152
1
2
0
15 cms
15
7,153
7153
1
1
0
3 cms
3
7,154
7154
1
1
0
3 cms
3
7,155
7155
1
1
0
5 cms
5
7,156
7156
1
1
0
6 cms
6
7,157
7157
1
1
0
5 cms
5
7,158
7158
1
1
0
5 cms
5
7,159
7159
1
1
0
5 cms
5
7,160
7160
1
1
0
7 cms
7
7,161
7161
1
1
0
5 cms
5
7,162
7162
1
2
0
12 cms
12
7,163
7163
1
1
0
6 cms
6
7,164
7164
1
1
0
2 cms
2
7,165
7165
1
1
0
5 cms
5
7,166
7166
1
1
0
3 cms
3
7,167
7167
1
1
0
2 cms
2
7,168
7168
1
1
0
4 cms
4
7,169
7169
1
1
0
5 cms
5
7,170
7170
1
1
0
3 cms
3
7,171
7171
1
1
0
5 cms
5
7,172
7172
1
1
0
5 cms
5
7,173
7173
1
1
0
4 cms
4
7,174
7174
1
1
0
3 cms
3
7,175
7175
1
1
0
4 cms
4
7,176
7176
1
1
0
7 cms
7
7,177
7177
1
1
0
3 cms
3
7,178
7178
1
1
0
5 cms
5
7,179
7179
1
1
0
4 cms
4
7,180
7180
1
1
0
6 cms
6
7,181
7181
1
1
0
3 cms
3
7,182
7182
1
1
0
3 cms
3
7,183
7183
1
1
0
2 cms
2
7,184
7184
1
1
0
3 cms
3
7,185
7185
1
1
0
4 cms
4