星期日 08:22:54 24.0360 84.7073 ↙234° 445 824 10,973 FlightAware ADS-B (PAT / VEPT) 星期日 08:23:25 23.9978 84.6494 ↙234° 444 822 10,973 FlightAware ADS-B (CCU / VECC) 星期日 08:23:56 23.9618 84.5950 ↙234° 446 826 10,973 FlightAware ADS-B (CCU / VECC) ...
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In a well tuned aircraft the desired and achieved roll and pitch should match to within a couple of degrees for any portion of the flight where stabilisation is enabled.</description> <expression>NAV_CONTROLLER_OUTPUT.nav_roll NAV_CONTROLLER_OUTPUT.nav_pitch degrees(ATTITUDE.roll) degrees(...
Status: Retired 1992. Gross mass: 85,800 kg (189,100 lb). Unfuelled mass: 4,400 kg (9,700 lb). Thrust: 866.71 kN (194,844 lbf). More at: Lox/KeroseneH-1-3 - Nissan solid rocket engine. Used on H-1 launch vehicle. First flight 1986. Status: Retired 1992. Number: 9 . ...
Apogee: 1,445 km (897 mi). Perigee: 264 km (164 mi). Inclination: 92.20 deg. Period: 102.10 min. Unusable orbit; would have been NOAA 7. At engine start up, one of the booster engines suffered an internal fuel leak, causing it to run at about 80% thrust. As a result the ...
The final Minuteman I (LGM-30B) R&D flight test missile (FTM 445) was launched from Cape Canaveral. This brought the total number of Minuteman IB launches to 36 - 31 from the Eastern Test Range and five from Vandenberg. A total of 67 Minuteman I (LGM-30A and LGM-30B) flight test mis...
inclination of 55 degrees was limited by range safety considerations. The circular orbit altitudes studied were in the range of 445 to 500 km. Orbit keeping propellant requirements increased rapidly at the lower bound and atmospheric protection from natural radiation fell off rapidly at higher ...
Bibliography: 102, 110, 2, 279, 376, 445, 474, 6, 7056, 13383. Photo Gallery Zenit-4MTCredit: Manufacturer Image1958 November 1 - . Vostok spacecraft and Zenit spy satellite authorised. - . Nation: Russia. Related Persons: Korolev. Spacecraft Bus: Vostok. Spacecraft: Vostok, Zenit-...
Flight: STS-51-D. Spacecraft Bus: Shuttle. Spacecraft: Discovery. Duration: 7.00 days. Decay Date: 1985-04-19 . USAF Sat Cat: 15641 . COSPAR: 1985-028A. Apogee: 535 km (332 mi). Perigee: 445 km (276 mi). Inclination: 28.50 deg. Period: 94.40 min. Manned seven crew. Payload...
Mass: 202 kg (445 lb). Nation: USA. Agency: USAF. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1966-12-31 . USAF Sat Cat: 2527 . COSPAR: 1966-099C. Apogee: 290 km (180 mi). Perigee: 287 km (178 mi). Inclination: 32.80 deg. Period: 90.30 min....