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Status: Retired 1999. First Launch: 1976-07-22. Last Launch: 1999-07-01. Number: 4 . Gross mass: 100 kg (220 lb). Thrust: 57.00 kN (12,814 lbf). Malenchenko, Yuri Ivanovich - Ukrainian pilot cosmonaut 1987-2016. Call sign: Agat (Agate). 827 cumulative days in space. Flight ...
Status: Study 1964. Thrust: 101,988.00 kN (22,927,814 lbf). More at: Lox/LH2Plug-Nozzle SASSTO - Notional LOx/LH2 rocket engine. Study 1967. Used on SASSTO launch vehicle. Status: Study 1967. Thrust: 1,574.90 kN (354,052 lbf). More at: Lox/LH2...
Perigee: 814 km (505 mi). Inclination: 45.01 deg. Period: 101.27 min. Plane C. Ascending node 181.7 degrees. Air dropped in Wallops Island DZ.. 1998 October 23 - . 00:02 GMT - . Launch Site: Cape Canaveral. Launch Complex: Mayport DZ. Launch Pad: 29.0 N x 78.3 W. Launch ...
Perigee: 814 km (505 mi). Inclination: 98.54 deg. Period: 101.22 min. Second dedicated Sterkh search-and-rescue satellite.. IRIS - . Nation: Russia. Agency: RKA. Class: Technology. Type: Technology satellite. USAF Sat Cat: 35867 . COSPAR: 2009-049C. Apogee: 502 km (311 mi). ...
Available add-ons Advanced Security Enterprise-grade security features GitHub Copilot Enterprise-grade AI features Premium Support Enterprise-grade 24/7 support Pricing Search or jump to... Search code, repositories, users, issues, pull requests... Provide feedback We read every piece of ...
Cosmos 814 - . Mass: 1,400 kg (3,000 lb). Nation: Russia. Agency: PKO. Class: Military. Type: Anti-satellite system. Spacecraft Bus: Kosmoplan. Spacecraft: IS-A. Decay Date: 1976-04-13 . USAF Sat Cat: 8806 . COSPAR: 1976-034A. Apogee: 480 km (290 mi). Perigee: 118 km ...
AKA: K.Status: Cancelled 1965.Gross mass: 12,000 kg (26,000 lb). These would include highly maneuverable high performance storable liquid propellant engine modules; nuclear reactor modules for high power space applications; ion engine units for inter-orbital transfer and interplanetary flight; and...
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Status: Study 1964. Thrust: 101,988.00 kN (22,927,814 lbf). More at: Lox/LH2Plug-Nozzle SASSTO - Notional LOx/LH2 rocket engine. Study 1967. Used on SASSTO launch vehicle. Status: Study 1967. Thrust: 1,574.90 kN (354,052 lbf). More at: Lox/LH2...