Sojuz 13
| Sojuz 13 (Союз-13) | |||
| Modell | Sojuz 7K-T | ||
|---|---|---|---|
| Anrop | Кавказ (Kavkaz - "Caucasus") | ||
| Färdens tid | 7 dag, 20 tim, 55 min, 35 sek | ||
| Massa | 6 560 kg | ||
| NSSDC-ID | 1973-103A[1] | ||
| Uppskjutning | |||
| Startplats | Bajkonur LC1 | ||
| Start | 18 december 1973, 11:55:00 UTC | ||
| Raket | Sojuz | ||
| Landning | |||
| Landningsplats | 200 km SW om Karaganda | ||
| Landning | 26 december 1973, 08:50:35 UTC | ||
| Omloppsbana | |||
| Varv | 127 st[2] | ||
| Apogeum | 247 km | ||
| Perigeum | 188 km | ||
| Banlutning | 51,6° | ||
| Besättning | |||
| Besättning | Valentin Lebedev (1)  Pyotr Klimuk (1) | ||
| Kronologi | |||
| |||
Sojuz 13 (ryska: Союз-13) var en flygning i det sovjetiska rymdprogrammet. Farkosten sköts upp med en Sojuz-raket från Kosmodromen i Bajkonur den 18 december 1973. För denna flygning hade man tagit bort omloppsmodulen och ersatt den med ett Orion 2 Rymdobservatorium. Farkosten återinträdde i jordens atmosfär och landade i Sovjetunionen den 26 december 1973.
Källor och referenser
- ^ ”NASA Space Science Data Coordinated Archive” (på engelska). NASA. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1973-103A. Läst 28 februari 2020.
- ^ Manned Astronautics - Figures & Facts Arkiverad 4 mars 2016 hämtat från the Wayback Machine., läst 8 oktober 2016.
| |||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
| |||||||||||||||||||||||||||||||||
Media som används på denna webbplats
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.
_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-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.
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).
Vostok spacecraft replica.jpg
Författare/Upphovsman: Pascal (Flickr user: pasukaru76), Licens: CC0
Vostok spacecraft replica at the Technik Museum Speyer, Germany.
Författare/Upphovsman: Pascal (Flickr user: pasukaru76), Licens: CC0
Vostok spacecraft replica at the Technik Museum Speyer, Germany.