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Contents

   



(Top)
 


1 Background  





2 Launch  





3 Orbit  





4 Scientific Instruments[5]  





5 See also  





6 References  














Kosmos 419






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From Wikipedia, the free encyclopedia
 


Kosmos 419
Mission typeMars orbiter
OperatorSoviet space program
COSPAR ID1971-042A Edit this at Wikidata
SATCAT no.5221
Mission duration2 days
Spacecraft properties
Spacecraft type3MS No. 170
ManufacturerNPO Lavochkin
Launch mass4,650 kg (10,250 lb)
Start of mission
Launch date10 May 1971, 16:58:42 (1971-05-10UTC16:58:42Z) UTC
RocketProton-K/D
Launch siteBaikonur 81/23
End of mission
DisposalLaunch failure
Decay date12 May 1971 (12 May 1971)
Orbital parameters
Reference systemGeocentric[1]
RegimeLow Earth
Perigee altitude134 km
Apogee altitude187 km
Inclination51.5°
Period87.7 min
Mars 2 →
 

Kosmos 419 (Russian: Космос 419 meaning Cosmos 419), also known as 3MS No.170 was a failed Soviet spacecraft intended to visit Mars. The spacecraft was launched on 10 May 1971, however, due to an upper stage malfunction, it failed to depart low Earth orbit.

Background[edit]

In 1971, Mars was at its closest to Earth since 1956, and in May of that year, both the Soviet Union and the United States made new attempts to reach the Red Planet. Kosmos 419 was intended to overtake the United States probes, Mariner 8 and Mariner 9, with the aim of becoming the first Mars orbiter. As it was, Mariner 8 was lost in a launch failure two days before Kosmos 419 was launched, and Mariner 9 went on to become the first spacecraft to orbit Mars.

Launch[edit]

Kosmos 419 was one of three Mars spacecraft launched by the Soviet Union in 1971, the others being Mars 2 and Mars 3; launched days after Kosmos 419. Unlike the 4M spacecraft, Mars 2 and 3, Kosmos 419 was a 3MS spacecraft which consisted only of an orbiter, with no lander.[2][3] It was the ninth Soviet spacecraft launched to Mars.

Orbit[edit]

A Proton-K carrier rocket successfully put the spacecraft and a Blok D upper stage into a low earth parking orbit with an apogee of 174 kilometres (108 mi) and a perigee of 159 kilometres (99 mi) and an inclination of 51.4 degrees. The Blok D's ignition timer was incorrectly set, resulting in it failing to ignite; the timer had been set so that the stage would ignite 1.5 years after launch rather than the intended 1.5 hours. Due to its low orbit, which quickly decayed, Kosmos 419 reentered the Earth's atmosphere on 12 May 1971, two days after launch.[4]

The designation Kosmos 419 was a generic name given to Soviet spacecraft operating in Earth orbit; at the time, Soviet planetary spacecraft which failed to depart Earth orbit would be given designations in the Kosmos series to disguise the failure.[4] Had it departed Earth orbit, Kosmos 419 would have become Mars 2, a designation which was used instead for the next mission, 4M No.171.

Scientific Instruments[5][edit]

  1. Fluxgate Magnetometer
  2. Infrared Radiometer
  3. Infrared Photometer
  4. Spectrometer
  5. Photometer
  6. Radiometer
  7. Ultraviolet Photometer
  8. Cosmic-ray detector
  9. Charged particle spectrometer
  10. Imaging System
  11. Stereo antenna

See also[edit]

References[edit]

  1. ^ Mark Wade. "Mars M-71". Encyclopedia Astronautica. Retrieved 2024-05-26.
  • ^ "Космические аппараты серии Марс-71 НПО им. С.А.Лавочкина". Laspace.ru. Archived from the original on 2013-05-10. Retrieved 2014-02-17.
  • ^ "Chronology of Mars Missions". ResearchGate. Archived from the original on 2018-12-10.
  • ^ a b "NASA—NSSDC—Spacecraft—Details". Nssdc.gsfc.nasa.gov. Retrieved 2014-02-17.
  • ^ "In Depth | Kosmos 419". Solar System Exploration: NASA Science. Retrieved 2018-12-26.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Kosmos_419&oldid=1232297009"

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    Mars program
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