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Kosmos 238

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Kosmos 238 (Russian: Космос 238 meaning Cosmos 238) was the final test series of the Soviet Soyuz spacecraft prior to the launch of Soyuz 2. It tested the orbital maneuvering system, reentry, descent and landing systems that had been modified and improved after the Soyuz 1 accident.

Mission parameters

  • Spacecraft: Soyuz 7K-OK
  • Mass: 6520 kg
  • Crew: None
  • Launched: 28 August 1968, 10:04:00 GMT
  • Landed: 1 September 1968, 09:03:00 GMT
  • Perigee: 194 km
  • Apogee: 313 km
  • Inclination: 51.7°
  • Period: 88.5 minutes
  • NSSDC ID: 1968-072A

References

Text comes from NASA NSSDC Master Catalog

Soyuz programme
Main topics
Past missions
(by spacecraft type)
Soyuz 7K-OK (1966–1970)
Soyuz 7K-L1 (1967–1970)
(Zond lunar programme)
Soyuz 7K-L1E (1969–1970)
Soyuz 7K-LOK (1971–1972)
Soyuz 7K-OKS (1971)
Soyuz 7K-T (1972–1981)
Soyuz 7K-TM (1974–1976)
Soyuz 7K-S (1974–1976)
Soyuz-T (1978–1986)
Soyuz-TM (1986–2002)
Soyuz-TMA (2002–2012)
Soyuz-TMA-M (2010–2016)
Soyuz MS (2016–present)
Current missions
Future missions
Uncrewed missions are designated as Kosmos instead of Soyuz; exceptions are noted "(uncrewed)".
The † sign designates failed missions. Italics designates cancelled missions.
← 1967Orbital launches in 19681969 →
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).


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