Venera 8

Venera 8
Assembly of Venera 8
Mission typeVenus lander
OperatorLavochkin
COSPAR ID1972-021A Edit this at Wikidata
SATCAT no.5912
Mission durationTravel: 117 days
Lander: 50 minutes
Spacecraft properties
Spacecraft4V-1 No.670
ManufacturerLavochkin
Launch mass1,184 kilograms (2,610 lb)[1]
Landing mass495 kilograms (1,091 lb)
Start of mission
Launch date27 March 1972, 04:15:06 (1972-03-27UTC04:15:06Z) UTC[1]
RocketMolniya-M/MVL
Launch siteBaikonur 31/6
End of mission
Last contact22 July 1972 (1972-07-23) at 09:32 UT (landing) + 50 min., 11 sec. when transmission ended
Orbital parameters
Reference systemGeocentric
Semi-major axis6,591 kilometres (4,095 mi)
Eccentricity0.03732
Perigee altitude194 kilometres (121 mi)
Apogee altitude246 kilometres (153 mi)
Inclination51.7°
Period88.9 minutes
Epoch27 March 1972
Venus lander
Landing date22 July 1972, 09:32 UTC
Landing site10°42′S 335°15′E / 10.70°S 335.25°E / -10.70; 335.25

Venera 8 (Russian: Венера-8 meaning Venus 8) was a probe in the Soviet Venera program for the exploration of Venus and was the second robotic space probe to conduct a successful landing on the surface of Venus.[2]

Venera 8 was a Venus atmospheric probe and lander. Its instrumentation included temperature, pressure, and light sensors as well as an altimeter, gamma ray spectrometer, gas analyzer, and radio transmitters.

  1. ^ a b Siddiqi, Asif (2018). Beyond Earth: A Chronicle of Deep Space Exploration, 1958–2016 (PDF) (second ed.). NASA History Program Office.
  2. ^ Harvey, Brian (2007). Russian Planetary Exploration History, Development, Legacy and Prospects. Springer-Praxis. pp. 115–118. ISBN 9780387463438.

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