Soyuz T-8

Soyuz T-8
COSPAR ID1983-035A Edit this at Wikidata
SATCAT no.14014
Mission duration2 days, 17 minutes, 48 seconds
Orbits completed32
Spacecraft properties
Spacecraft typeSoyuz-T
ManufacturerNPO Energia
Launch mass6,850 kilograms (15,100 lb)
Crew
Crew size3
MembersVladimir Titov
Gennady Strekalov
Aleksandr Serebrov
CallsignOkean (Ocean)
Start of mission
Launch dateApril 20, 1983, 13:10:54 (1983-04-20UTC13:10:54Z) UTC
RocketSoyuz-U
Launch siteBaikonur 1/5
End of mission
Landing dateApril 22, 1983, 13:28:42 (1983-04-22UTC13:28:43Z) UTC
Landing site60 kilometres (37 mi) NE of Arkalyk
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude200 kilometres (120 mi)
Apogee altitude230 kilometres (140 mi)
Inclination51.6 degrees
Period88.6 minutes
Soyuz programme
(Crewed missions)

Soyuz T-8 was a crewed mission to the Salyut 7 Soviet space station in 1983. Shortly into the mission, the spacecraft failed to dock with the space station[1] due to an incident involving an antenna being torn off the craft by the protective launch shroud. After a fuel-consuming attempt made in darkness for an optical rendezvous with Salyut 7 resulted in an abort in order to avoid collision, it was decided to de-orbit T-8 two days into the mission in order to ensure that the spacecraft had a sufficient amount of propellant for the de-orbit maneuver. After de-orbiting, landing of the craft occurred normally.

  1. ^ Yenne, Bill (1988). The Pictorial History of World Spaceflight. Exeter. p. 158. ISBN 0-7917-0188-3.