Mars Global Surveyor

Mars Observer and Mars Global Surveyor
Mars Global Surveyor is the name given to a small orbiter, to be
launched in November 1996, that will recover some of the science goals
of the lost Mars Observer mission.
MGS will be roughly half the mass and size of Mars Observer. The
image above shows both spacecraft in their mapping configurations.
(It was rendered at MSSS from our own preliminary models and is not
"official".)
Press Releases
Instrument Selection
The instruments selected for Mars Global Surveyor are the Mars Orbital
[previously, Observer] Camera (MSSS/Caltech), the Thermal Emission
Spectrometer (Arizona State University/Hughes Santa Barbara Research
Center), the Mars Orbiter [previously, Observer] Laser Altimeter (NASA
Goddard Space Flight Center), the Magnetometer/Electron Reflectometer
(GSFC), and the Mars Relay [previously, Mars Balloon Relay] (French
National Center for Space Exploration, CNES). Radio science will also
be done, via an Ultrastable Oscillator in the spacecraft's downlink
subsystem.
The other two instruments on Mars Observer, the Gamma Ray Spectrometer
(UofA/MMAG) and the Pressure-Modulator Infrared Radiometer (JPL), will
be flown on a small orbiter to be launched in 1998.
Mars Orbital Camera
The Mars Orbital Camera (Mars Global Surveyor Orbiter Camera), or MOC
2, is the spare instrument fabricated during the Mars Observer
mission. The investigation's science objectives, hardware
implementation, ground data system, and science analysis plans are
essentially identical to those of the Mars Observer investigation. These are described in a
series of papers published prior to the loss of Mars Observer.
Additional materials available include:
Spacecraft Selection
The Request For Proposals for the spacecraft was issued in early
April, and responses were received in mid-May. On 8 July, JPL
announced that Martin Marietta Technologies Inc. of Denver, Colorado,
had been selected to build Mars Global Surveyor.
MGS Project WWW Server
Mars Global Surveyor Project
server at JPL
MGS Timetable
-
3 to 24 Nov 1996
- Launch on Delta II 7925
- 10 to 27 Sep 1997
- Mars Orbit Insertion into capture orbit
-
Oct 1997 to Jan 1998
- aerobraking to 380-km circular mapping orbit
- late Jan 1998
- Mapping mission starts
Preliminary
version of the MGS Mission Plan