Cosmos 482

Launch Partial Failure

Liftoff Time (GMT)

04:02:00

Friday March 31, 1972

Mission Details

Launch Notes

Last flight of Molniya-M /Block-NVL.

Cosmos 482

Cosmos 482 (Russian: Космос 482 meaning Cosmos 482), launched March 31, 1972, at 04:02:33 UTC, was an attempted Venus probe which failed to escape low Earth orbit. It reentered Earth's atmosphere on May 10, 2025, at 6:24 UTC and fell into the Indian Ocean. Its landing module, which weighs 495 kilograms (1,091 lb), is highly likely to reach the surface of Earth in one piece as it was designed to withstand 300g of acceleration and 100 atmospheres of pressure. Beginning in 1962, the name Kosmos was given to Soviet spacecraft which remained in Earth orbit, regardless of whether that was their intended final destination. The designation of this mission as an intended planetary probe is based on evidence from Soviet and non-Soviet sources and historical documents. Typically Soviet planetary missions were initially put into an Earth parking orbit as a launch platform with a rocket engine and attached probe. The probes were then launched toward their targets with an engine burn with a duration of roughly four minutes. If the engine misfired or the burn was not completed, the probes would be left in Earth orbit and given a Kosmos designation. Cosmos 482 was launched by a Molniya booster on March 31, 1972, four days after the Venera 8 atmospheric probe and may have been similar in design and mission plan. After achieving an Earth parking orbit, the spacecraft made an apparent attempt to launch into a Venus transfer trajectory. It separated into four pieces, two of which remained in low Earth orbit and decayed within 48 hours into south New Zealand (known as the Ashburton balls incident), and two pieces (presumably the payload and detached engine unit) went into a higher 210 x 9,800 km orbit. An incorrectly set timer caused the Blok L stage to cut off prematurely, preventing the probe from escaping Earth orbit.

Heliocentric Orbit

1 Payload

1,180 kilograms

Rocket

Retired
Molniya-M/Block NVL

Active 1970 to 1992

RKK Energiya logo

Manufacturer

RKK Energiya

Rocket

Height: 44.63m

Payload to Orbit

LEO: 6,200 kg

GTO: 2,400 kg

Liftoff Thrust

4,391 Kilonewtons

Fairing

Diameter: 2.58m

Height: 7.14m

Stages

4

Strap-ons

4

Launch Site

Site 31/6

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

47 hr 9 min

Stats

Molniya-M


32nd

Mission

2nd

Mission of 1972

RKK Energiya


16th

Mission of 1972

1972


24th

Orbital launch attempt