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Luna 22

Soviet lunar orbiter


Soviet lunar orbiter

FieldValue
nameLuna 22
mission_typeLunar orbiter
operatorSoviet space program
COSPAR_ID1974-037A
SATCAT7315
mission_duration
spacecraft_busYe-8-LS
manufacturerGSMZ Lavochkin
launch_mass5700 kg
launch_dateUTC
launch_rocketProton-K/D
launch_siteBaikonur 81/24
deactivatedEarly
orbit_referenceSelenocentric
orbit_periapsis219 km
orbit_apoapsis222 km
orbit_inclination19.35 degrees
orbit_period130 minutes
orbit_semimajor6598.3 km
orbit_eccentricity0.18
apsisselene
typeorbiter
objectLunar
orbits~3,875
arrival_date2 June 1974
location
programmeLuna programme
previous_missionLuna 21
next_missionLuna 23

Luna 22 (Ye-8-LS series) was an uncrewed space mission, part of the Soviet Luna program, also called Lunik 22.

Overview

Luna 22 was a lunar orbiter mission. The spacecraft carried imaging cameras and also had the objectives of studying the Moon's magnetic field, surface gamma ray emissions and composition of lunar surface rocks, and the gravitational field, as well as micrometeorites and cosmic rays. Luna 22 was launched into Earth parking orbit and then to the Moon. It was inserted into a circular lunar orbit on 2 June 1974. The spacecraft made many orbit adjustments over its 18-month lifetime in order to optimize the operation of various experiments, lowering the perilune to as little as 25 km.

Luna 22 was the second of two "advanced" lunar orbiters, the first of which being Luna 19 . The orbiter was designed to conduct extensive scientific surveys from orbit. Well in route to the Moon, Luna 20 had to perform a single mid-course correction on 30 May, and entered lunar orbit on 2 June 1974. When the orbiter first entered orbit of the Moon, it started at periapsis altitude at 219 km and apoapsis altitude as 222 km, and an inclination of 19°35', these orbital parameters changed throughout its mission. Throughout the orbiters various orbital changes, Luna 22 had performed without any problems, and it continued to return photos fifteen months into its mission, past the conclusion of its primary mission, which had ended by 2 April 1975. The maneuvering propellant on the spacecraft was depleted on 2 September 1975, and the mission was formally concluded in early November 1975, following a highly successful mission.

References

Info: Wikipedia Source

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