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Status: Operational 2014.First Launch: 2014-10-23.Last Launch: 2014-10-23.Number: 1 .Gross mass: 14 kg (30 lb).Apogee: 381,280 km (236,910 mi). More at:4M. Family Communications Country Launch Vehicles Chang Zheng 3C/G2 Bibliography ...
Status: Study 1963. Gross mass: 700,000 kg (1,540,000 lb). Unfuelled mass: 250,000 kg (550,000 lb). Thrust: 6,860.00 kN (1,542,180 lbf). More at: Nuclear/LH2N1 Nuclear AF - Russian nuclear orbital launch vehicle. A variant of the first alternative considered in the 1963 ...
First flight 1965. Polysulfide binder with aluminum binder fuel in case of high strength steel with a graphite throat insert. Status: Out of Production. Date: 1962-1966. Gross mass: 150 kg (330 lb). Unfuelled mass: 33 kg (72 lb). Thrust: 46.00 kN (10,341 lbf). More at: SolidT-...
Perigee: 873 km (542 mi). Inclination: 64.80 deg. Period: 103.40 min. Ocean surveillance; nuclear powered; test flight of modified safer design.. 1980 November 4 - . 15:04 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: R-36. ...
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Thrust (vac): 6,860.000 kN (1,542,180 lbf). Isp: 425 sec. Burn time: 260 sec. Isp(sl): 330 sec. Diameter: 9.15 m (30.01 ft). Span: 9.15 m (30.01 ft). Length: 38.72 m (127.03 ft). Propellants: Lox/LH2. No Engines: 1. Engine: Plug-Nozzle J-2. Status: Study 1993. ...
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...