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Mars Observer Mars-orbiter spacecraft family

The Mars Observer family comprised the 1992 NASA Mars orbiter designed to map the planet surface, atmosphere, climate, and magnetic environment; contact was lost during the planned orbit-insertion sequence.

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Identity

Aliases
Mars ObserverMO
Family Name
Mars Observer
Full Name
Mars Observer Mars-orbiter spacecraft family
Roles
interplanetary_probeorbiter
Status
retired
Type
spacecraft

Details

Description
The Mars Observer family comprised the 1992 NASA Mars orbiter designed to map the planet surface, atmosphere, climate, and magnetic environment; contact was lost during the planned orbit-insertion sequence.
First Flight Year
1,992
Last Flight Year
1,993
Operator
Propulsion Configurations
  • Entries
    • Count
      1
      Propulsion System
      Role
      maneuvering
      Stage
      spacecraft
      Variant Notes
      Four 490 N MMH/NTO bipropellant engines for trajectory-correction maneuvers, Mars orbit insertion, and large spacecraft velocity changes.
    • Count
      1
      Propulsion System
      Role
      attitude-control
      Stage
      spacecraft
      Variant Notes
      Four 22 N MMH/NTO bipropellant engines for finer trajectory control and pitch/yaw control.
    • Count
      1
      Propulsion System
      Role
      maneuvering
      Stage
      spacecraft
      Variant Notes
      Eight 4.45 N catalytic hydrazine engines for reaction-wheel momentum desaturation and orbit-trim maneuvers.
    • Count
      1
      Propulsion System
      Role
      attitude-control
      Stage
      spacecraft
      Variant Notes
      Four 0.9 N catalytic hydrazine engines for roll control.
    Name
    Mars Observer dual-mode bipropellant and hydrazine propulsion installation
    Notes
    NASA identifies four 490 N and four 22 N MMH/NTO bipropellant engines for trajectory control, orbit insertion, and pitch/yaw control, plus eight 4.45 N and four 0.9 N hydrazine monopropellant engines for reaction-wheel desaturation, orbit trim, and roll control.
Spacecraft Specs
Launch Mass Kg
1,018

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Creation Time
August 6, 2026 at 17:41:47 UTC
Updated Time
September 8, 2026 at 09:48:29 UTC