Polyot

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Polyot 11A59
Fact sheet
Function Interim carrier rocket
Manufacturer OKB-1
Country of origin Soviet Union
Size
Height 30m (98ft)
Diameter 2.99m (9.8ft)
Mass 277,000kg (610,000lb)
Stages 1
Capacity
Payload to LEO 1,400kg (3,000lb)
Launch History
Status Retired
Launch Sites LC-31, Baikonur
Total launches 2
Successes 2
Maiden flight 1 November 1963
Last flight 12 April 1964
Boosters (Stage 0)
No boosters 4
Engines 1 RD-107-8D74K
Thrust 995.3kN (223,752lbf)
Specific Impulse 257 sec
Burn time 119 seconds
Fuel RP-1/LOX
First Stage
Engines 1 RD-0108
Thrust 294kN (66,093lbf)
Specific Impulse 330 sec
Burn time 240 seconds
Fuel RP-1/LOX

The Polyot was an interim orbital carrier rocket, built to test ASAT spacecraft. It was required as a stopgap after the cancellation of the UR-200 programme, but before the Tsiklon could enter service. Only two were ever launched, the first on 1 November 1963, and the last on 12 April 1964. Both of these flights were successful.

The rocket consisted of a core stage, and four boosters, which were taken from a Voskhod 11A57 rocket. It was capable of delivering a 1,400kg payload into a 300km by 59o Low Earth orbit.

It is a member of the R-7 family.

Contents

[edit] See also

[edit] Comparable rockets

[edit] Related developments

[edit] Associated spacecraft

[edit] External links

Encyclopedia Astronautica entry

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Soviet (to 1991) and Russian expendable launch vehicles
Active: Cosmos-3M | Dnepr | Molniya | Proton | Rockot | Shtil' | Soyuz (U, 2) | START-1 | Strela | Tsyklon | Volna | Zenit
In Development: Angara | Onega
Past: Energia | N1 | Polyot | R-7 Semyorka | Voskhod | Vostok