Encyclopedia Astronautica
Kosmos 63S1M

Kosmos LV
Credit: © Mark Wade
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
Ukrainian orbital launch vehicle. Modernized version of 63S1 initial configuration of the first Kosmos launcher and the prototype for the production 11K63 launch vehicle. Suborbital launches from Plesetsk from 1965 at from the modified R-12 silo 'Dvina'. Flown only a few times in 1965-1967. Succeeded by the 11K63 production model launched from the 'Raduga' complex.

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.

AKA: Kosmos 2M; 63S1M; SL-7; Sandal; B-1.
Status: Out of production.
Gross mass: 48,110 kg (106,060 lb).
Payload: 450 kg (990 lb).
Height: 25.80 m (84.60 ft).
Diameter: 1.60 m (5.20 ft).
Thrust: 636.50 kN (143,091 lbf).
Apogee: 270 km (160 mi).

More... - Chronology...

Associated Countries
Associated Spacecraft
  • DS-P1-Yu Ukrainian military target satellite. 79 launches, 1964.07.30 (Cosmos 36) to 1976.08.26 (Cosmos 850). Development of systems for air defense and the control of outer space. More...
  • DS-U2-V Ukrainian military technology satellite. 4 launches, 1965.10.19 (Cosmos 93) to 1968.02.20 (Cosmos 202). Military technology development satellite - mission still classified. More...
  • DS-U2-M Ukrainian technology satellite. 2 launches, 1965.11.26 (Cosmos 97) to 1967.03.03 (Cosmos 145). Development tests of atomic clocks. More...
  • DS-P1-I Ukrainian military target satellite. 19 launches, 1966.01.25 (Cosmos 106) to 1977.06.18 (Cosmos 919). Operational radar target for the ABM forces. More...

Associated Engines
  • RD-119 Glushko lox/udmh rocket engine. 105.5 kN. Kosmos 1 stage 2. Out of production. Isp=352s. Derived from RD-109 motor originally intended for the second stage of a Lox/UDMH version of the R-7. First flight 1961. More...
  • RD-214 Glushko Nitric acid/Kerosene rocket engine. 730 kN. R-12, Kosmos 11K63 stage 1. Isp=264s. Single turbopump driven by H2O2 gas generator feeding four fixed chambers. Ignition with propellant TG-02. First flight 1957. More...

See also
  • Kosmos 2 In 1960 the Soviet government decreed development of a lightweight launch vehicle for launch of payloads not requiring R-7 family of boosters. A modification of the R-12 IRBM was selected as the first stage; a new high-performance second stage was developed using a unique Lox/UDMH propellant combination. After two failures, the first successful flight was on March 16, 1962. More...

Associated Manufacturers and Agencies
  • Yuzhnoye Ukrainian manufacturer of rockets, spacecraft, and rocket engines. Yangel Design Bureau, Dnepropetrovsk, Ukraine. More...

Associated Stages
  • Kosmos A-1 Nitric acid/Kerosene propellant rocket stage. Loaded/empty mass 39,515/3,150 kg. Thrust 730.50 kN. Vacuum specific impulse 264 seconds. More...
  • S1 Lox/UDMH propellant rocket stage. Loaded/empty mass 8,595/840 kg. Thrust 105.51 kN. Vacuum specific impulse 352 seconds. More...

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