Soyuz 16

Soyuz 16
Mission typeOrbital test flight
OperatorSoviet space program
COSPAR ID1974-096A Edit this at Wikidata
SATCAT no.7561
Mission duration5 days, 22 hours and 23 minutes
Orbits completed95
Spacecraft properties
SpacecraftSoyuz 7K-TM No.4
Spacecraft typeSoyuz 7K-TM
ManufacturerNPO Energia
Launch mass6,680 kg (14,730 lb)[1]
Landing mass1,200 kg (2,600 lb)
Crew
Crew size2
MembersAnatoly Filipchenko
Nikolai Rukavishnikov
CallsignБуран (Buran - "Blizzard")
Start of mission
Launch date2 December 1974, 09:40:00 UTC
RocketSoyuz-U
Launch siteBaikonur 1/5[2]
End of mission
Landing date8 December 1974, 08:03:35 UTC
Landing site30 km (19 mi) of the northeast of Arkalyk, Kazakhstan
Orbital parameters
Reference systemGeocentric orbit[3]
RegimeLow Earth orbit
Perigee altitude177 km (110 mi)
Apogee altitude223 km (139 mi)
Inclination51.7°
Period88.4 minutes

Soviet stamp featuring Filipchenko and Rukavishnikov (1975)

Soyuz 16 (Russian: Союз 16, Union 16) was a December, 1974, crewed test flight for a joint Soviet-United States space flight which culminated in the Apollo–Soyuz mission in July 1975. The two-man Soviet crew, Anatoly Filipchenko and Nikolai Rukavishnikov, tested a docking ring and other systems to be used in the joint flight.

  1. ^ Cite error: The named reference Display was invoked but never defined (see the help page).
  2. ^ "Baikonur LC1". Encyclopedia Astronautica. Archived from the original on 15 April 2009. Retrieved 4 March 2009.
  3. ^ Cite error: The named reference Trajectory was invoked but never defined (see the help page).