Kosmos 359
Mission type | Venus lander[1] |
---|---|
Operator | Lavochkin |
COSPAR ID | 1970-065A |
SATCAT no. | 04501 |
Mission duration | Launch failure |
Spacecraft properties | |
Spacecraft type | 3MV |
Manufacturer | Lavochkin |
Launch mass | 1,180 kilograms (2,600 lb) |
Start of mission | |
Launch date | 22 August 1970, 05:06:09 | UTC
Rocket | Molniya-M 8K78M |
Launch site | Baikonur 31/6 |
End of mission | |
Decay date | 6 November 1970 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Eccentricity | 0.05041 |
Perigee altitude | 210 kilometres (130 mi) |
Apogee altitude | 910 kilometres (570 mi) |
Inclination | 51.5 degrees |
Period | 95.70 minutes |
Venera → |
Kosmos 359 was an unmanned Soviet
Design
The lander was designed to be able to survive atmospheric pressures of up to 180 bars (18,000 kPa) and temperatures of 580 °C (1,076 °F).[6] This was significantly greater than what was expected to be encountered, but significant uncertainties as to the surface temperatures and pressure of Venus resulted in the designers opting for a large margin of error.[6] The degree of hardening added mass to the probe, which limited the amount of mass available for scientific instruments on the probe and the interplanetary bus.[6]
Rocket malfunction
After reaching orbit, the main upper stage engine ignited late and shut down early after running for only twenty-five seconds. The error was ultimately attributed to an error in the DC transformer of the power supply system.[5]
Experiments
Kosmos 359 carried a limited set of scientific instruments, including a solar wind detector, cosmic-ray detector, resistance thermometer, and aneroid barometer.[5]
See also
References
- ^ Krebs, Gunter. "Interplanetary Probes". Gunter's Space Page. Retrieved 31 October 2016.
- ISBN 978-1-4419-7897-4.
- .
- ^ Morov, V. I.; Bazilevsky, A. T. (2003). Space Science and Technology.
- ^ LCCN 2017059404. SP2018-4041.
- ^ ISBN 9781441978974.