LLMpediaThe first transparent, open encyclopedia generated by LLMs

Luna 21

Generated by DeepSeek V3.2
Note: This article was automatically generated by a large language model (LLM) from purely parametric knowledge (no retrieval). It may contain inaccuracies or hallucinations. This encyclopedia is part of a research project currently under review.
Article Genealogy
Expansion Funnel Raw 46 → Dedup 0 → NER 0 → Enqueued 0
1. Extracted46
2. After dedup0 (None)
3. After NER0 ()
4. Enqueued0 ()
Luna 21
NameLuna 21
Mission typeLunar lander and rover
OperatorGSKB Spetsmash
COSPAR ID1973-001A
SATCAT06333
Mission durationTravel: 7 days Lander: ~4 months Rover: ~4 months
SpacecraftYe-8 No.204
ManufacturerLavochkin
Launch mass5,700 kg (12,600 lb)
Landing mass1,836 kg (4,048 lb)
Launch date8 January 1973, 06:55:38 UTC
Launch rocketProton-K/D
Launch siteBaikonur 81/24
Last contactRover: 10 May 1973 Lander: 3 June 1973
Lunar landing15 January 1973, 22:35 UTC
Landing siteLe Monnier crater, Mare Serenitatis
Distance driven42 km (26 mi)
ProgrammeLuna programme
Previous missionLuna 20
Next missionLuna 22

Luna 21 was a highly successful robotic space mission of the Soviet space program that delivered the Lunokhod 2 rover to the Moon. Launched in January 1973, it was part of the long-running Luna programme and represented a major advancement in planetary surface exploration. The mission significantly extended the operational and scientific achievements of its predecessor, Lunokhod 1, conducting extensive studies of the lunar surface and its environment.

Mission overview

The primary objective of Luna 21 was to deploy a second, improved Lunokhod rover on the Moon to conduct detailed scientific exploration. Managed by the design bureau Lavochkin, the mission aimed to continue the Soviet Union's dominance in automated lunar roving following the success of Lunokhod 1. Key goals included high-resolution panoramic imaging, analysis of surface soil mechanics, measurements of X-ray and ultraviolet solar radiation, and precise laser ranging experiments. The target landing site was the eastern edge of Mare Serenitatis, within Le Monnier crater, an area of significant geological interest.

Spacecraft design

The Luna 21 spacecraft consisted of two main components: a lander stage and the Lunokhod 2 rover. The lander, based on the robust Ye-8 bus, served as a delivery and communications platform, equipped with dual ramps for rover egress. The Lunokhod 2 rover was an enhanced version of its predecessor, with a more sophisticated suite of instruments. Its payload included three television cameras, a RIFMA X-ray fluorescence spectrometer, a X-ray telescope, an astrophotometer to measure sky brightness, a mechanical penetrometer, a laser retroreflector, and a radiation detector. The rover's improved design allowed for greater speed and maneuverability on the lunar surface.

Journey and lunar landing

Launched on a Proton-K rocket from Baikonur Cosmodrome on 8 January 1973, Luna 21 followed a direct trajectory to the Moon. After a midcourse correction, the spacecraft entered lunar orbit on 12 January. Following orbit adjustments, the descent engine fired, and the lander successfully touched down on 15 January at 22:35 UTC on the floor of Le Monnier crater. The landing site, at coordinates 25.85° N, 30.45° E, placed the mission on the border between the Mare Serenitatis basaltic plains and the surrounding highland terrain. Within hours, the Lunokhod 2 rover successfully descended to the surface via one of the lander's ramps.

Lunokhod 2 operations

Lunokhod 2 began its traverses immediately, operated by a driver team at the Soviet deep space communication center near Simferopol in the Crimea. Over its operational life, the rover far exceeded its design expectations, traveling a total of 42 kilometers across the lunar surface, a record for extraterrestrial roving that stood for decades. It conducted systematic soil analyses, took over 86 panoramic images, and performed numerous mechanical tests with its penetrometer. The rover navigated around craters, investigated rilles, and traversed the highland margins, providing invaluable data on surface geology and topography. Operations ceased on 10 May 1973, after the rover's electronics likely overheated when soil covered its radiator during a crater exploration.

Scientific results and legacy

The mission returned a wealth of scientific data, including over 80,000 television images and detailed chemical analyses of the regolith. The RIFMA spectrometer confirmed the basaltic composition of Mare Serenitatis and detected variations in aluminum and silicon content. The laser retroreflector continues to be used for Earth-Moon distance measurements by observatories like the Apache Point Observatory. Lunokhod 2's marathon drive provided critical insights into soil properties and trafficability for future missions. The mission cemented the Soviet space program's leadership in robotic lunar exploration and its technological legacy directly informed later planetary rover designs, including those for Mars. The Lunokhod 2 rover itself became a subject of historical interest when its location was identified in 2010 from Lunar Reconnaissance Orbiter imagery, and its retroreflector was used for fresh scientific measurements.

Category:Luna programme Category:Spacecraft launched in 1973 Category:Missions to the Moon