Venera 12

Venera 12
Venera 12 model
OperatorSoviet Academy of Sciences
COSPAR ID1978-086A
1978-086C
SATCAT no.11025
12028
Mission durationTravel: 3 months and 6 days
Lander: 110 minutes
Spacecraft properties
Spacecraft type4V-1
Bus4MV
Launch mass4,457.9 kg (9,828 lb)
Dry mass1,600 kg (3,500 lb)
Dimensions2.3 m × 2.7 m × 5.7 m (7.5 ft × 8.9 ft × 18.7 ft)
Start of mission
Launch date14 September 1978, 02:25:13 UTC
RocketProton-K/D-1 8K82K
Launch siteBaikonur 81/23
End of mission
Last contact18 April 1980
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Semi-major axis6,569 kilometres (4,082 mi)
Perigee altitude177 kilometres (110 mi)
Apogee altitude205 kilometres (127 mi)
Inclination51.5°
Flyby of Venus
Spacecraft componentVenera 12 flight platform
Closest approach19 December 1978
Distance~35,000 kilometers (22,000 mi)
Venus lander
Spacecraft componentVenera 12 descent craft
Landing date21 December 1978, 03:30
Landing site7°S 294°E / 7°S 294°E / -7; 294

The Venera 12 (Russian: Венера-12 meaning Venus 12) was an uncrewed Soviet space mission designed to explore the planet Venus. Venera 12 was launched on 14 September 1978 at 02:25:13 UTC.

After separating from its flight platform on 19 December 1978, the Venera 12 lander entered the Venus atmosphere two days later at 11.2 kilometres per second (7.0 mi/s). During its descent, the lander employed aerodynamic braking followed by parachute braking, ending with atmospheric braking. After a nearly one-hour descent, a soft landing was made at 06:30 Moscow time (0330 UT) on 21 December. Touchdown speed was 7–8 metres per second (23–26 ft/s); landing coordinates are 7°S 294°E / 7°S 294°E / -7; 294. After touchdown, the lander transmitted data to the flight platform for about 110 minutes until the flight platform, which remained in a heliocentric orbit, moved out of range. Venera 11 and 12 carried identical instruments.