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
| |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Media som används på denna webbplats
Soyuz 7K-OK(A) drawing.png
Soyuz 7K-OK(A) spacecraft with an active docking unit.
Soyuz 7K-OK(A) spacecraft with an active docking unit.
Soyuz-TM drawing.png
Soyuz-TM spacecraft. Compare the antennas on the orbital module to those on Soyuz-T. Differences reflect the change from the Igla rendezvous system used on Soyuz-T to the Kurs rendezvous system used on Soyuz-TM.
Soyuz-TM spacecraft. Compare the antennas on the orbital module to those on Soyuz-T. Differences reflect the change from the Igla rendezvous system used on Soyuz-T to the Kurs rendezvous system used on Soyuz-TM.
_drawing.png)
Soyuz 7K-TM (APAS) drawing.png
Apollo-Soyuz Test Project (ASTP) Soyuz. The APAS-75 docking unit is located at left.
Apollo-Soyuz Test Project (ASTP) Soyuz. The APAS-75 docking unit is located at left.
Soyuz TMA-04M rocket on the launch pad.jpg
The Soyuz TMA-04M spacecraft is seen after being rolled out by train to the launch pad at the Baikonur Cosmodrome in Kazakhstan, May 13, 2012. The launch of the Soyuz spacecraft, with Expedition 31 Soyuz Commander Gennady Padalka, Flight Engineer Sergei Revin of Russia and NASA Flight Engineer Joe Acaba, is scheduled for 9:01 a.m., May 15 (Kazakhstan time).
The Soyuz TMA-04M spacecraft is seen after being rolled out by train to the launch pad at the Baikonur Cosmodrome in Kazakhstan, May 13, 2012. The launch of the Soyuz spacecraft, with Expedition 31 Soyuz Commander Gennady Padalka, Flight Engineer Sergei Revin of Russia and NASA Flight Engineer Joe Acaba, is scheduled for 9:01 a.m., May 15 (Kazakhstan time).
Soyuz-A drawing.png
Soyuz-A manned spacecraft concept (1963). It was to have been part of the Soyuz A-B-C circumlunar complex.
Soyuz-A manned spacecraft concept (1963). It was to have been part of the Soyuz A-B-C circumlunar complex.