Launch Date March 27, 1969
Launch Site Baikonur Cosmodrome, Kazakhstan, Russia | Launch Site 81L
Destination Mars
Type Orbiter
Status Unsuccessful
Nation Soviet Union
Alternate Names N/A

Goals

The spacecraft was design to study Mars from orbit.

Accomplishments

None. The launch vehicle failed and the probe never reached Earth orbit.

In Depth

The M-69 series of Mars spacecraft was the first of a new generation of Mars probes designed by the Lavochkin design bureau for launch on the heavy Proton booster. The probes were designed around a single large spherical tank to which three pressurized compartments were attached. Although the 1969 missions were originally meant for both Mars orbit and landing, weight constraints late in mission design forced engineers to delete the lander and focus only on a Mars orbit mission.

After two en route midcourse corrections, the spacecraft were intended to enter orbit around Mars at roughly 1,700 x 34,000 kilometers at 40 degree inclination. After an initial photography mission, the probes would lower their pericenters to about 500 to 700 kilometers for a second imaging mission. Total mission lifetime would be about three months. During the launch of the first M-69, the Proton's third stage stopped firing at T+438.66 seconds, after its turbopump had caught on fire because of a faulty rotor bearing. The probe, scheduled to reach Mars orbit on 11 September 1969, never reached Earth orbit.

Spacecraft

Launch Vehicle: 8K82K + Blok D (Proton no. 240-01)

Spacecraft Mass: 3,800 kiolgrams

Spacecraft Instruments:

  1. radiometer
  2. instrument to measure water vapor levels
  3. ultraviolet spectrometer
  4. radiation detector
  5. gamma spectrometer
  6. hydrogen/helium mass spectrometer
  7. spectrometer
  8. low-energy ion spectrometer
  9. imaging system (three cameras)

Selected References

Siddiqi, Asif A. Deep Space Chronicle: A Chronology of Deep Space and Planetary Probes 1958-2000, NASA, 2002.

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