Luna 13
| Operator | Soviet Union |
|---|---|
| Major contractors | GSMZ Lavochkin |
| Mission type | Planetary Science Lunar landing |
| Launch date | 21 December 1966 10:17:00 UTC |
| Carrier rocket | Molniya 8K78M (4-Stage R-7/SS-6) |
| Launch site | Baikonur Cosmodrome |
| Mission duration | 6 days. Last transmission 28 December 1966 06:13 UTC. |
| COSPAR ID | 1966-116A |
| Mass | 1,620 kg (3,600 lb) |
| Moon landing | |
| Date | 24 December 1966 18:04 UTC |
| Coordinates | 18°52'N 62°3'W |
| Instruments | |
| Main instruments | Stereo photographic imaging system Infrared radiometer Penetrometer Radiation densitometer Radiation detector |
| References: NASA NSSDC Master Catalog | |
Luna 13 (E-6M series) was an unmanned space mission of the Luna program, also called Lunik 13.
The Luna 13 spacecraft was launched toward the Moon from an earth-orbiting platform and accomplished a soft landing on December 24, 1966, in the region of Oceanus Procellarum.
The petal encasement of the spacecraft was opened, antennas were erected, and radio transmissions to Earth began four minutes after the landing. On December 25 and December 26, 1966, the spacecraft television system transmitted panoramas of the nearby lunar landscape at different Sun angles. Each panorama required approximately 100 minutes to transmit. The spacecraft was equipped with a mechanical soil-measuring penetrometer, a dynamograph, and a radiation densitometer for obtaining data on the mechanical and physical properties and the cosmic ray reflectivity of the lunar surface. Transmissions from the spacecraft ceased on December 28, 1966.
Luna 13 became the third spacecraft to successfully soft-land on the surface of the Moon (after Luna 9 and the American Surveyor 1). The probe landed in the Ocean of Storms at 18:01 UT on 24 December 1966, between the Krafft and Seleucus craters at 18°52' north latitude and 62°3' west longitude. Unlike its predecessor, the heavier Luna 13 lander (113 kilograms) carried a suite of scientific instruments in addition to the usual imaging system.
A three-axis accelerometer within the pressurized frame of the lander recorded the landing forces during impact to determine the soil structure down to a depth of 20 to 30 centimeters. A pair of spring-loaded booms was also deployed. One of these booms carried a penetrometer, designed to measure the forces required to penetrate the lunar regolith – the penetrating force being supplied by a minute explosive charge. The other boom carried a backscatter densitometer that was used to infer the density of the lunar near-surface regolith. Four radiometers recorded infrared radiation from the surface indicating a noon temperature of 117 ±3 °C while a radiation detector indicated that radiation levels would be less than hazardous for humans.
The lander returned a total of five panoramas of the lunar surface, showing a more smooth terrain than seen by Luna 9. One of the two cameras (intended to return stereo images) failed, but this did not diminish the quality of the photographs. After a fully successful mission, contact was lost at 06:13 UTC on 28 December when the on-board batteries were exhausted.
| Preceded by Luna 12 |
Luna programme | Succeeded by Luna 1968A |
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