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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 . ...
Status: Development ended 1988. Gross mass: 248,100 kg (546,900 lb). Unfuelled mass: 10,820 kg (23,850 lb). More at: Lox/Kerosene/LH2MAKS-D - Russian winged orbital launch vehicle. NPO Molniya, Antonov, and TsAGI proposed a spaceplane demonstrator project to the European Space ...
Status: Development 1988. Stage 2. 1 x MAKS Tank. Gross Mass: 248,000 kg (546,000 lb). Empty Mass: 11,000 kg (24,000 lb). Isp: 437 sec. Burn time: 440 sec. Isp(sl): 396 sec. Diameter: 6.38 m (20.93 ft). Span: 6.38 m (20.93 ft). Length: 32.10 m (105.30 ft). ...
. Status: Retired 1998. Gross mass: 25,649 kg (56,546 lb). Unfuelled mass: 3,733 kg (8,229 lb). Thrust: 577.34 kN (129,791 lbf). More at: Nitric acid/UDMHTaepodong 1-2 - Nitric acid/UDMH propellant rocket stage. Included 100 kg spin table for spin-up of third stage prior...
Mass: 248 kg (546 lb). Nation: USA. Agency: NASA Greenbelt. Class: Earth. Type: Atmosphere satellite. Spacecraft Bus: T100. Spacecraft: TOMS-EP. USAF Sat Cat: 23940 . COSPAR: 1996-037A. Apogee: 746 km (463 mi). Perigee: 705 km (438 mi). Inclination: 98.30 deg. Period: 99.30...
Apogee: 20,192 km (12,546 mi). Perigee: 20,174 km (12,535 mi). Inclination: 55.00 deg. Period: 718.00 min. Third GPS Block IIF satellite, spacecraft 65; replaced SVN 39 in the Navstar constellation. The upper stage and payload first entered a 163 km x 394 km x 41.6 deg ...
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Apogee: 546 km (339 mi). Perigee: 144 km (89 mi). Inclination: 65.10 deg. Period: 91.40 min. ASAT interceptor. Succeeded in intercept of Cosmos 1375 target. Deorbited using on-board engine. Final test of series.. 1982 August 30 - . 10:06 GMT - . Launch Site: Baikonur. Launch ...