Sojuz 16
| Sojuz 16 (Союз-16) | |||
 | |||
| Modell | Sojuz 7K-TM | ||
|---|---|---|---|
| Anrop | Буран (Buran - "Blizzard") | ||
| Färdens tid | 5 dag, 22 tim, 23 min, 35 sek | ||
| Massa | 6 800 kg | ||
| NSSDC-ID | 1974-096A[1] | ||
| Uppskjutning | |||
| Startplats | Bajkonur 1/5 | ||
| Start | 2 december 1974, 09:40:00 UTC | ||
| Raket | Sojuz-U | ||
| Landning | |||
| Landningsplats | 30 km NÖ om Arkalyk | ||
| Landning | 8 december 1974, 08:03:35 UTC | ||
| Omloppsbana | |||
| Varv | 95 st[2] | ||
| Sträcka | 3,98 miljoner km | ||
| Apogeum | 291 km | ||
| Perigeum | 184 km | ||
| Banlutning | 51,8° | ||
| Besättning | |||
| Besättning | Anatoli Filipchenko  (2)Nikolai Rukavishnikov (2) | ||
| Kronologi | |||
| |||
Sojuz 16 (ryska: Союз-16) var en flygning i det sovjetiska rymdprogrammet. Farkosten sköts upp med en Sojuz-U-raket från Kosmodromen i Bajkonur den 2 december 1974 Flygningen var det första bemannade test av den version av Sojuz farkost som skulle användas i samarbetsprojektet ASTP. Farkosten återinträdde i jordens atmosfär och landade i Sovjetunionen den 8 december 1974.
Källor och referenser
- ^ ”NASA Space Science Data Coordinated Archive” (på engelska). NASA. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1974-096A. Läst 28 februari 2020.
- ^ Manned Astronautics - Figures & Facts Arkiverad 4 mars 2016 hämtat från the Wayback Machine., läst 8 oktober 2016.
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Media som används på denna webbplats
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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.
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Apollo-Soyuz Test Project (ASTP) Soyuz. The APAS-75 docking unit is located at left.
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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.
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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).
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Författare/Upphovsman: Pascal (Flickr user: pasukaru76), Licens: CC0
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Författare/Upphovsman: Pascal (Flickr user: pasukaru76), Licens: CC0
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