Sojuz 2
| Sojuz 2 (Союз-2) | |||
_drawing.png) | |||
| Modell | Sojuz 7K-OK | ||
|---|---|---|---|
| Färdens tid | 3 dagar | ||
| Massa | 6 450 kg | ||
| NSSDC-ID | 1968-093A[1] | ||
| Uppskjutning | |||
| Startplats | Bajkonur 1/5 | ||
| Start | 25 oktober 1968, 09:00 UTC | ||
| Raket | Sojuz | ||
| Landning | |||
| Landning | 28 oktober 1968, 07:51 UTC | ||
| Omloppsbana | |||
| Varv | 48 st | ||
| Apogeum | 229 km | ||
| Perigeum | 191 km | ||
| Banlutning | 51,7° | ||
| Kronologi | |||
| |||
Sojuz 2 (ryska: Союз-2) var en obemannad flygning i det sovjetiska rymdprogrammet.[2] Farkosten sköts upp från Kosmodromen i Bajkonur[3], den 25 oktober 1968 med en Sojuz-raket. Planen var att den skulle docka med den bemannade Sojuz 3. Farkosterna tog som planerat in på varandra, men någon dockning genomfördes aldrig.[4] Farkosten återinträdde i jordens atmosfär och landade på jorden den 28 oktober 1968.
Referenser
- Den här artikeln är helt eller delvis baserad på material från engelskspråkiga Wikipedia, tidigare version.
Noter
- ^ ”NASA Space Science Data Coordinated Archive” (på engelska). NASA. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1968-093A. Läst 28 februari 2020.
- ^ Fredrik von Scheele och Johan Warell. ”Sojuz”. Nationalencyklopedin. Bokförlaget Bra böcker AB, Höganäs. http://www.ne.se/uppslagsverk/encyklopedi/l%C3%A5ng/sojuz. Läst 24 juni 2015.
- ^ ”Baikonur LC1” (på engelska). Encyclopedia Astronautica. Arkiverad från originalet den 15 april 2009. https://web.archive.org/web/20090415160730/http://www.astronautix.com/sites/baiurlc1.htm. Läst 24 juni 2015.
- ^ Asif. A. Siddiqi (2000) (på engelska). Challenge to Apollo: The Soviet Union and the Space Race, 1945-1974. NASA. sid. 345. http://history.nasa.gov/SP-4408pt1.pdf. Läst 24 juni 2015
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