|Mission type||Mars orbiter|
|Mission duration||7 months 3 days (launch to last contact)|
|Launch mass||3440 kg|
|Start of mission|
|Launch date||25 July 1973, 18:55:48UTC|
|Launch site||Baikonur 81/24|
|End of mission|
|Last contact||28 February 1974|
|Periareon altitude||1,760 kilometres (1,090 mi)|
|Apoareon altitude||32,586 kilometres (20,248 mi)|
|Epoch||12 February 1974|
|Orbital insertion||12 February 1974, 15:45 UTC|
Mars 5 (Russian: Марс-5), also known as 3MS No.53S was a Soviet spacecraft launched to explore Mars. A 3MS spacecraft launched as part of the Mars programme, it successfully entered orbit around Mars in 1974. However, it failed a few weeks later.
The Mars 5 spacecraft carried an array of instruments to study Mars. In addition to cameras, it was equipped with a radio telescope, an IR radiometer, multiple photometers, polarimeters, a magnetometer, plasma traps, an electrostatic analyser, a gamma-ray spectrometer, and a radio probe. The Three cameras were a 52mm Vega, a 350mm Zulfar and a panoramic camera.
Built by Lavochkin, Mars 5 was the second of two 3MS spacecraft launched to Mars in 1973, following Mars 4. A 3MS was also launched during the 1971 launch window as Kosmos 419. However, due to a launch failure, it failed to depart Earth orbit. In addition to the orbiters, two 3MP lander missions, Mars 6 and Mars 7, were launched during the 1973 window.
Mars 5 was launched by a Proton-K carrier rocket with a Blok D upper stage, flying from Baikonur Cosmodrome Site 81/24. The launch occurred at 18:55:48 UTC on 25 July 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 5 into heliocentric orbit bound for Mars.
The spacecraft performed course correction manoeuvres on 3 August 1973 and 2 February 1974.
The probe reached Mars on 12 February. At 14:44:25 the spacecraft's engines ignited to begin its orbit insertion burn, which successfully placed it into an Areocentric orbit with a periapsis of 1,760 kilometres (1,090 mi), an apoapsis of 32,586 kilometres (20,248 mi), and 35.3 degrees inclination.
The spacecraft's pressurised instrument compartment began to leak as soon as the spacecraft entered orbit around Mars, which controllers believed to be the result of a micrometeoroid impact during orbital insertion. It ceased operations on 28 February, having returned 180 photographic frames, 43 of which were of usable quality. The probe's original planned lifetime in mars orbit has been 3 months. The probe's gamma ray spectrometer measured the uranium, thorium and potassium content of the surface the probe passed over and found they were similar to Igneous rocks on earth. The exact ratios of the elements varied with the age of the surface. Mars 5's Infrared radiometer reported a daytime surface temperature of between -44°C and -2°C. Night time temperatures were measured at -73°C.
- Krebs, Gunter. "Interplanetary Probes". Gunter's Space Page. Retrieved 12 April 2013.
- "Mars 5". Retrieved 6 December 2018.
- McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 12 April 2013.
- "Mars 5". US National Space Science Data Centre. Retrieved 12 April 2013.
- Siddiqi, Asif A. (2002). "1973". Deep Space Chronicle: A Chronology of Deep Space and Planetary Probes 1958-2000 (PDF). Monographs in Aerospace History, No. 24. NASA History Office. pp. 101–106.
- Harvey, Brian (2007). Russian Planetry Exploration History, Development, Legacy and Prospects. Springer-Praxis. p. 154. ISBN 9780387463438.
- Harvey, Brian (2007). Russian Planetry Exploration History, Development, Legacy and Prospects. Springer-Praxis. pp. 161–165. ISBN 9780387463438.