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Sputnik 11A59
Part of R-7
Russian orbital launch vehicle. Two stage version of Vostok 11A57. Used for flight test of prototype Chelomei ASAT after cancellation of UR-200 booster and before availability of Tsyklon.
AKA: 11A59;A;Polyot;SL-10. Status: Retired 1964. First Launch: 1963-11-01. Last Launch: 1964-04-12. Number: 2 . Payload: 1,400 kg (3,000 lb). Thrust: 3,999.93 kN (899,220 lbf). Gross mass: 277,000 kg (610,000 lb). Height: 30.00 m (98.00 ft). Diameter: 2.99 m (9.80 ft). Apogee: 300 km (180 mi).
LEO Payload: 1,400 kg (3,000 lb) to a 300 km orbit at 59.00 degrees.
Family:
orbital launch vehicle.
Country:
Russia.
Engines:
RD-107-8D74K,
RD-108-8D75K.
Spacecraft:
Polyot.
Launch Sites:
Baikonur,
Baikonur LC31.
Stages:
Voskhod 11A57-0,
Voskhod 11A57-1.
Agency:
Korolev bureau.
1963 November 1 - .
08:56 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Sputnik 11A59.
1964 April 12 - .
09:21 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC31.
LV Family:
R-7.
Launch Vehicle:
Sputnik 11A59.
- Polet 2; Polyot 2 - .
Payload: I-2B s/n 2. Mass: 1,400 kg (3,000 lb). Nation: Russia.
Agency: Korolev bureau.
Class: Military.
Type: Anti-satellite system. Spacecraft Bus: Kosmoplan.
Spacecraft: Polyot.
Decay Date: 1966-06-08 . USAF Sat Cat: 783 . COSPAR: 1964-019A. Apogee: 479 km (297 mi). Perigee: 303 km (188 mi). Inclination: 58.10 deg. Period: 92.30 min. ASAT interceptor control and propulsion test. Elaboration of systems providing for the extensive manouevring of space apparatuses..
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