Luna 22

Launch Success

Liftoff Time (GMT)

08:56:00

Wednesday May 29, 1974

Mission Details

Luna 22

Wiki

Luna 22 (Ye-8-LS series) was an unmanned space mission, part of the Soviet Luna program, also called Lunik 22. 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. Maneuvering fuel was exhausted on 2 September and the mission was ended in early November. Luna 22 was the second of two "advanced" lunar orbiters (the first being Luna 19) designed to conduct extensive scientific surveys from orbit. Launched about a year after the termination of Lunokhod 2 operations on the lunar surface, Luna 20 performed a single mid-course correction en route the Moon on 30 May before entering lunar orbit on 2 June 1974. Initial orbital parameters were 219 × 222 kilometers at 19°35' inclination. In addition to its primary mission of surface photography, Luna 22 also performed investigations to determine the chemical composition of the lunar surface, recorded meteoroid activity, searched for a lunar magnetic field, measured solar and cosmic radiation flux, and continued studies of the irregular magnetic field. Through various orbital changes, Luna 22 performed without any problems and continued to return photos fifteen months into the mission, although its primary mission had ended by 2 April 1975. The spacecraft's maneuvering propellant was finally depleted on 2 September, and the highly successful mission was formally terminated in early November 1975.

Lunar orbit

1 Payload

5,700 kilograms

Rocket

Retired
Proton-K/Block D

Active 1967 to 1976

Khrunichev State Research and Production Space Center logo

Manufacturer

Khrunichev

Rocket

Height: 56.14m

Payload to Orbit

LEO: 18,900 kg

GTO: 9,000 kg

Liftoff Thrust

8,840 Kilonewtons

Fairing

Diameter: 3.9m

Height: 8.9m

Stages

4

Launch Site

Site 81/24

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

6 days

Stats

Proton-K


42nd

Mission

2nd

Mission of 1974

Khrunichev State Research and Production Space Center


840th

Mission

30th

Mission of 1974

1974


40th

Orbital launch attempt