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Sputnik 8A91
Part of R-7
R-7 aft end
Credit: © Mark Wade
Russian intercontinental ballistic orbital launch vehicle. Modified R-7 ICBM used to launch Sputnik 3.
AKA: 8A91;A;SL-2. Status: Retired 1958. First Launch: 1958-04-27. Last Launch: 1958-05-15. Number: 2 . Payload: 1,327 kg (2,925 lb). Thrust: 3,784.90 kN (850,879 lbf). Gross mass: 269,300 kg (593,700 lb). Height: 31.10 m (102.00 ft). Diameter: 2.99 m (9.80 ft). Span: 9.76 m (32.02 ft). Apogee: 217 km (134 mi).
LEO Payload: 1,327 kg (2,925 lb) to a 217 km orbit at 65.00 degrees. Flyaway Unit Cost 1985$: 33.000 million.
More at: Sputnik 8A91.
Family:
ICBM,
orbital launch vehicle.
Country:
Russia.
Engines:
RD-107-8D76,
RD-108-8D77.
Spacecraft:
Sputnik 3.
Launch Sites:
Baikonur,
Baikonur LC1.
Stages:
R-7A 8K74-1,
Vostok 8A92-0.
Agency:
Korolev bureau.
1958 April 27 - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Sputnik 8A91.
FAILURE: Launch vehicle disintegrated 88 seconds after liftoff..
Failed Stage: 0.
- Sputnik failure - .
Payload: D-1 s/n 1. Mass: 1,327 kg (2,925 lb). Nation: Russia.
Agency: MVS.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: Sputnik 3.
Decay Date: 1958-04-01 .
1958 May 15 - .
07:00 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC1.
LV Family:
R-7.
Launch Vehicle:
Sputnik 8A91.
- Sputnik 3 - .
Payload: D-1 s/n 2. Mass: 1,327 kg (2,925 lb). Nation: Russia.
Agency: MVS.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: Sputnik 3.
Decay Date: 1960-04-06 . USAF Sat Cat: 8 . COSPAR: 1958-Delta-2. Apogee: 1,864 km (1,158 mi). Perigee: 217 km (134 mi). Inclination: 65.20 deg. Period: 106.00 min. Variety of scientific data. Research in the upper atmosphere and outer space.
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