Astronomy:Mars 7
 | |
| Mission type | Mars flyby/lander[1] |
|---|---|
| Operator | Lavochkin |
| COSPAR ID | Bus: 1973-053A Lander: 1973-053D[2] |
| SATCAT no. | Bus: 6776 Lander: 7224[2] |
| Mission duration | 7 months (launch to nearest approach) |
| Spacecraft properties | |
| Spacecraft | 3MP No.51P |
| Manufacturer | Lavochkin |
| Launch mass | 3,260 kg (fueled lander and bus)[2] |
| Start of mission | |
| Launch date | 9 August 1973, 17:00:17 UTC[3] |
| Rocket | Proton-K/D |
| Launch site | Baikonur 81/24 |
| End of mission | |
| Last contact | 25 March 1974[4] |
| Orbital parameters | |
| Reference system | Heliocentric |
| Flyby of Mars | |
| Spacecraft component | Bus |
| Closest approach | 9 March 1974 |
| Mars flyby (failed landing) | |
| Spacecraft component | Lander |
| Closest approach | 9 March 1974 |
| Distance | 1,300 km (810 mi) |
Mars 7 (Russian: Марс-7), also known as 3MP No.51P was a Soviet spacecraft launched in 1973 to explore Mars. A 3MP bus spacecraft which comprised the final mission of the Mars programme, it consisted of a lander and a coast stage with instruments to study Mars as it flew past. Due to a malfunction, the lander failed to perform a maneuver necessary to enter the Martian atmosphere, missing the planet and remaining in heliocentric orbit along with the coast stage.
Spacecraft
Mars 7 spacecraft carried an array of instruments to study Mars. The lander was equipped with a thermometer and barometer to determine the surface conditions, an accelerometer and radio altimeter for descent, and instruments to analyse the surface material including a mass spectrometer.[5] The coast stage, or bus, carried a magnetometer, plasma traps, cosmic ray and micrometeoroid detectors, stereo antennae, and an instrument to study proton and electron fluxes from the Sun.[5]
Built by Lavochkin, Mars 7 was the second of two 3MP spacecraft launched to Mars in 1973, having been preceded by Mars 6. Two orbiters, Mars 4 and Mars 5, were launched earlier in the 1973 Mars launch window and were expected to relay data for the two landers. However, Mars 4 failed to enter orbit, and Mars 5 failed after a few days in orbit.
Launch
Mars 7 was launched by a Proton-K carrier rocket with a Blok D upper stage, flying from Baikonur Cosmodrome Site 81/24.[3] The launch occurred at 17:00:17 UTC on 9 August 1973, with the first three stages placing the spacecraft and upper stage into a low Earth parking orbit before the Blok D fired to propel Mars 7 into heliocentric orbit bound for Mars. The spacecraft performed a course correction on 16 August 1973.[5]
Mars 7's lander separated from the flyby bus on 9 March 1974. Initially, it failed to separate. However, it was eventually released to begin its descent. Due to a retrorocket failure, the probe missed the atmosphere of Mars, and, instead of landing, flew past along with the coast stage, with a closest approach of 1,300 km (810 mi).[5] Known faults with the spacecraft's transistors were blamed for the failure, along with that of Mars 4.[5]
See also
References
- ↑ Krebs, Gunter. "Interplanetary Probes". Gunter's Space Page. http://space.skyrocket.de/doc_sat/ip_probe.htm.
- ↑ 2.0 2.1 2.2 "Mars 7". US National Space Science Data Centre. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1973-053A.
- ↑ 3.0 3.1 McDowell, Jonathan. "Launch Log". Jonathan's Space Page. http://planet4589.org/space/log/launchlog.txt.
- ↑ Asif A. Siddiqi. "Beyond Earth : A CHRONICLE OF DEEP SPACE EXPLORATION, 1958–2016" (PDF). https://www.nasa.gov/sites/default/files/atoms/files/beyond-earth-tagged.pdf.
- ↑ 5.0 5.1 5.2 5.3 5.4 Siddiqi, Asif A. (2002). "1973". Deep Space Chronicle: A Chronology of Deep Space and Planetary Probes 1958-2000. Monographs in Aerospace History, No. 24. NASA History Office. pp. 101–106. https://history.nasa.gov/monograph24/1973.pdf.
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