NEXT SPACEFLIGHT

Status

Failure

M-69 n°522

Launch Time
Wed Apr 02, 1969 10:33 UTC

Two seconds after the launch, one of the RD-253 engines explodes. The launcher however continues its flight, but after 25 seconds, it tilts, and crashes at 3 kilometers from the launch pad.

Rocket

Proton-K/Block D
RVSN USSR
Status: Retired
Liftoff Thrust: 8,840 kN
Payload to LEO: 18,900 kg
Payload to GTO: 9,000 kg
Stages: 4
Strap-ons: 0
Rocket Height: 56.14 m
Fairing Diameter: 3.9 m
Fairing Height: 8.9 m

Mission Details

M-69 n°522

The Mars M-69 probes were originally intended to consist of both an orbiter and a lander. Time constraints did not permit the development of a soft lander, so engineers decided to simply use a hard lander that would crash into the Martian surface but gather data during its descent.

At first, a modified Luna Ye-8 bus was to be used for the spacecraft, however it had a number of limitations that made it unsuitable for the long journey to Mars. Halfway through the project, Lavochkin Bureau design chief Georgi Babakin decided to simply discard the Luna E-8 derived probe and design a completely new one from scratch.

However, the 2M probes ended significantly heavier than intended and engineers also ran out of time to conduct drop tests of the lander, so that part was abandoned which left only the orbiter. If successful, this would still be a major propaganda success for the Soviets as NASA was nearly three years away from attempting a Mars orbiter.

Payloads: 1
Total Mass: 4,850.0 kg
Heliocentric Orbit

Location

Site 81/24, Baikonur Cosmodrome, Kazakhstan

Stats

1969

38th orbital launch attempt

Proton-K

13th mission
4th mission of 1969
7th failed mission