Luna 10 mockup, Le Bourget (France) | |
Mission type | Lunar orbiter |
---|---|
Operator | Soviet space program |
COSPAR ID | 1966-027A |
SATCAT no. | 02126 |
Mission duration | 60 days |
Spacecraft properties | |
Spacecraft type | E-6S |
Manufacturer | GSMZ Lavochkin |
Launch mass | 1,583.7 kg[1] |
Dry mass | 540 kg |
Start of mission | |
Launch date | 31 March 1966, 10:46:59 UTC[1] |
Rocket | Molniya-M 8K78M |
Launch site | Baikonur, Site 31/6 |
End of mission | |
Last contact | 30 May 1966 |
Orbital parameters | |
Reference system | Selenocentric |
Periselene altitude | 349 km |
Aposelene altitude | 1015 km |
Inclination | 71.9° |
Period | 178.05 minutes |
Lunar orbiter | |
Orbital insertion | 3 April 1966, 18:44 GMT |
Instruments | |
Magnetometer Gamma-ray spectrometer Five gas-discharge counters Two ion traps/charged particle trap Piezoelectric micrometeorite detector Infrared detector Low-energy x-ray photon counters | |
Luna 10 (or Lunik 10) was a 1966 Soviet lunar robotic spacecraft mission in the Luna program. It was the first artificial satellite of the Moon.[1]
Luna 10 conducted extensive research in lunar orbit, gathering important data on the strength of the Moon's magnetic field,[2] its radiation belts, and the nature of lunar rocks (which were found to be comparable to terrestrial basalt rocks),[3] cosmic radiation, and micrometeoroid density. Perhaps its most important finding was the first evidence of mass concentrations (called "mascons") — areas of denser material below the lunar surface that distort lunar orbital trajectories.[4][5][6]
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