 |
| Mission type | Test Flight |
|---|---|
| Operator | Experimental Design Bureau (OKB-1) |
| Orbits completed | Failed to orbit |
| Spacecraft properties | |
| Spacecraft | Soyuz 7K-OK No.1 |
| Spacecraft type | Soyuz 7K-OK |
| Manufacturer | Experimental Design Bureau (OKB-1) |
| Launch mass | 6316 kg [1] |
| Landing mass | 2505 kg |
| Dimensions | 7.13 m long 2.72 m wide |
| Start of mission | |
| Launch date | 14 December 1966 11:00 GMT[1] |
| Rocket | Soyuz 11A511 s/n U15000-01 |
| Launch site | Baikonur, Site 31 |
| Contractor | Experimental Design Bureau (OKB-1) |
| End of mission | |
| Landing date | 14 December 1966 18 December 1966 (planned) |
| Landing site | 400 m of the pad 31 Kazakh Steppe, Kazakhstan (planned) |
Soyuz 7K-OK No.1 was an uncrewed spacecraft of the Soyuz programme, originally intended to perform a rendezvous maneouvre with Kosmos 133 (Soyuz 7K-OK No.2). After the Kosmos 133 mission failed, the rocket was moved to the launch pad on 12 December 1966 and scheduled to launch on 14 December 1966, 11:00 GMT.[2][1]
- ^ a b c "From bad to worse: Soyuz disaster". RussianSpaceWeb.com. 27 June 2019. Retrieved 20 October 2020.
- ^ Первушин, Антон Иванович; Pervushin, Anton Ivanovich (2014). Звездные войны. СССР против США [Star Wars: USSR versus USA)] (in Russian). ISBN 978-5-367-03181-2.