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Kosmos 63S1M
 Kosmos LV Credit: © Mark Wade |
AKA: 63S1M;B-1;Kosmos 2M;SL-7. Status: Out of production. Payload: 450 kg (990 lb). Thrust: 636.50 kN (143,091 lbf). Gross mass: 48,110 kg (106,060 lb). Height: 25.80 m (84.60 ft). Diameter: 1.60 m (5.20 ft). Apogee: 270 km (160 mi).
LEO Payload: 450 kg (990 lb) to a 270 km orbit at 71.00 degrees.
Stage Data - Kosmos 63S1M
- Stage 1. 1 x Kosmos A-1. Gross Mass: 39,515 kg (87,115 lb). Empty Mass: 3,150 kg (6,940 lb). Thrust (vac): 730.500 kN (164,223 lbf). Isp: 264 sec. Burn time: 125 sec. Isp(sl): 230 sec. Diameter: 1.60 m (5.20 ft). Span: 1.80 m (5.90 ft). Length: 18.00 m (59.00 ft). Propellants: Nitric acid/Kerosene. No Engines: 1. Engine: RD-214. Other designations: Sandal; SS-4; 8K63; R-12; 63; 11K63. Status: Out of Production.
- Stage 2. 1 x Kosmos A-2. Gross Mass: 8,595 kg (18,948 lb). Empty Mass: 840 kg (1,850 lb). Thrust (vac): 105.510 kN (23,720 lbf). Isp: 352 sec. Burn time: 250 sec. Isp(sl): 220 sec. Diameter: 1.60 m (5.20 ft). Span: 1.60 m (5.20 ft). Length: 7.80 m (25.50 ft). Propellants: Lox/UDMH. No Engines: 1. Engine: RD-119. Other designations: S1. Status: Out of Production.
Family: orbital launch vehicle. Country: Ukraine. Engines: RD-214, RD-119. Spacecraft: DS-P1-Yu, DS-U2-V, DS-U2-M, DS-P1-I. Stages: S1, Kosmos A-1. Agency: Yuzhnoye.
 | R-56, R-26, 63S1 From left to right, dynamic test models of: R-56 monster launch vehicle; R-26 ICBM; Kosmos 63S1 launch vehicle Credit: © Mark Wade |
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