Luna 24

Launch Success

Liftoff Time (GMT)

15:04:12

Monday August 9, 1976

Mission Details

Luna 24

Wiki

Luna 24 was a robotic probe of the Soviet Union's Luna programme. The last of the Luna series of spacecraft, the mission of the Luna 24 probe was the third Soviet mission to return lunar soil samples from the Moon (the first two sample return missions were Luna 16 and Luna 20). The probe landed in Mare Crisium (Sea of Crises). The mission returned 170.1 g of lunar samples to the Earth on 22 August 1976. Luna 24 was based on the Ye-8-5 spacecraft body, consisting of two attached stages, an ascent stage mounted on top of a descent stage. The lander stood 3.96 meters tall and had an unfueled landed mass of 1880 kg. With a full load of fuel its launch mass was between 5600 and 5750 kg. The descent stage was the same as the Ye-8 lower stage for the Lunokhod rovers, a cylindrical body with four protruding landing legs, fuel tanks, a landing radar altimeter, and a dual descent engine complex. The main descent rocket, the KTDU-417, was a throttleable 1920 kg thrust engine used for mid-course corrections, orbit insertion, braking for descent to the surface, and to slow the craft until it reached a cutoff point which was determined by the onboard computer based on altitude and velocity. After cutoff a bank of lower thrust (210 and 350 kg) vernier jets was used for the final landing. The descent stage also acted as a launch pad for the ascent stage. The spacecraft descent stage was equipped with a television camera, radiation and temperature monitors, telecommunications equipment, and a 90 cm extendable arm with a drilling rig for the collection of a lunar soil sample. Communications were via a conical antenna at the end of a boom at 768 and 922 MHz (downlink) and 115 MHz (uplink).

Trans Lunar Injection

1 Payload

5,797 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 81/23

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

11 days 23 hours

Stats

Proton-K


53rd

Mission

2nd

Mission of 1976

Khrunichev State Research and Production Space Center


1048th

Mission

59th

Mission of 1976

1976


82nd

Orbital launch attempt