Mars 1M No.1

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1M No.1
Mars 1M.jpg
A Mars 1M spacecraft
Mission typeMars flyby
Mission durationFailed to orbit
Spacecraft properties
Spacecraft typeMars 1M
ManufacturerOKB-1 RSC-Energia
Launch mass650 kilograms (1,430 lb)
Start of mission
Launch date10 October 1960, 14:27:49 (1960-10-10UTC14:27:49Z) UTC
RocketMolniya 8K78/L1-4M Modified SS-6
Launch siteBaikonur 1/5
Instruments
1) Ultraviolet Spectrograph

2) Radiation Detector 3) Cosmic-Ray Detector 4) Television Imaging System (Removed)

5) Spectroreflectometer (Removed)
 

Mars 1M No.1, designated Mars 1960A by NASA analysts and dubbed Marsnik 1 by the Western media, was the first spacecraft launched as part of the Soviet Union's Mars programme.[1] A Mars 1M spacecraft, it was intended for conducting flight testing system and to study the interplanetary environment between Earth and Mars, however it was lost in a launch failure before it could begin its mission.[2][3]

Launch[edit]

Mars 1M No.1 was the payload of the Molniya 8K78 rocket's maiden flight. The rocket, which had serial number L1-4M, was a new derivative of the R-7 series, with a Blok-I third stage replacing the Blok-E used on the Vostok, and a new Blok-L fourth stage. The vehicle lifted off from Site 1/5 at the Baikonur Cosmodrome at 14:27:49 UTC on 10 October 1960.[4][5]

Scientific Instruments[6][edit]

  • Ultraviolet Spectrometer
  • Radiation Detector
  • Cosmic-Ray Detector
  • Television Imaging System (Removed)
  • Spectroreflectometer (Removed)

Television Imaging System and Spectroreflectometer were removed due to mass constraints.

End of mission[edit]

It was delineated that during the course of second stage of flight, the resonant vibration in third stage of rocket provoked by malfunction of gyroscope and it damaged the attitude control system of carrier rocket. The flight was persecuted by multitudinous vibrations generated by synergy of upper stage booster. Following this issue, the horizon sensor disconnected from the booster and the rocket descended from normal flight path angle. As a consequence the rocket’s third stage commanded to stop ignition after five minutes into flight, during this stage the spacecraft uplifted to an altitude of 120km before re-entry. Thereafter, the spacecraft re-entered and disintegrated in LEO and its debris fallen over Siberia with 4,800 km down range. It failed to achieve low earth orbit.[7][8]

See also[edit]

References[edit]

  1. ^ Zak, Anatoly. "Russia's unmanned missions to Mars". RussianSpaceWeb. Retrieved 26 October 2013.
  2. ^ Krebs, Gunter. "Mars 1M". Gunter's Space Page. Retrieved 26 October 2013.
  3. ^ Wade, Mark. "Mars 1M". Encyclopedia Astronautica. Retrieved 26 October 2013.
  4. ^ McDowelll, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 26 October 2013.
  5. ^ "(PDF) Chronology of Mars Missions". ResearchGate. Retrieved 2018-12-09.
  6. ^ "In Depth | 1M/1". Solar System Exploration: NASA Science. Retrieved 2018-12-09.
  7. ^ "The Space Review: The beginnings of planetary exploration: the first probes to Venus". www.thespacereview.com. Retrieved 2018-12-09.
  8. ^ "Mars 1M satellite". weebau.com. Retrieved 2018-12-09.