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Fobos 1 Mission Information

From Nick Greene, for About.com

Fobos 1 Mission to Mars

Fobos 1 Mission to Mars

NASA
Key Dates:
  • 07.07.88 Launch
  • 09.02.88 Contact Lost
  • 11.03.88 End of Mars Mission
  • Status: Contact Lost
Planetary Studies Experiments (on Orbiter):
  1. VSK videospectrometric system
  2. ISM infrared spectrometer
  3. GS-14 gamma-emission spectrometer
  4. IPNM neutron detector
  5. RLK radar system
  6. LIMA-D laser mass spectrometric analyzer
  7. DION secondary ion mass analyzer
  8. ISO optical radiation spectrometer
Plasma Studies Experiments:
  1. MAGMA magnetometer
  2. FGMM magnetometer
  3. APV-F plasma wave analyzer
  4. ASPERA scanning energy-mass spectrometer
  5. SOVIKOMS energy-mass charge spectrometer
  6. TAUS proton and alpha-particle spectrometer
  7. HARP ion and electron spectrometer
  8. SLED energetic charged-particle spectrometer
Solar Studies Experiments:
  1. IPHIR solar photometer
  2. TEREK solar telescope/coronograph
  3. RF-15 x-ray photometer
  4. SUFR ultrasound spectrometer
  5. LILAS gamma-burst spectrometer
  6. VGS gamma-burst spectrometer
Fobos 1 Mission Information: Fobos 1, and its companion spacecraft Fobos 2, were the next-generation in the Venera-type planetary missions, succeeding those last used during the Vega 1 and 2 missions to comet P/Halley. Each spacecraft, with a newly designed bus, carried twenty-four experiments provided by thirteen countries and the European Space Agency. The objectives of the Fobos missions were to: (1) conduct studies of the interplanetary environment; (2) perform observations of the Sun; (3) characterize the plasma environment in the Martian vicinity; (4) conduct surface and atmospheric studies of Mars; and, (5) study the surface composition of the Martian satellite Phobos.

The main section of the spacecraft consisted of a pressurized toroidal electronics section surrounding a modular cylindrical experiment section. Below these were mounted four spherical tanks containing hydrazine for attitude control and, after the main propulsion module was to be jettisoned, orbit adjustment. A total of 28 thrusters (twenty-four 50 N thrusters and four 10 N thrusters) were mounted on the spherical tanks with additional thrusters mounted on the spacecraft body and solar panels. Attitude was maintained through the use of a three-axis control system with pointing maintained with sun and star sensors.

Fobos 1 performed a course correction en route to Mars on 16 July 1988. On 29 August 1988, due to a programming error, a command was issued to turn off the orientation and stabilization system (instead of a routine command to switch on the gamma-ray spectrometer). Fobos 1 operated nominally until an expected communications session on 2 September 1988 failed to occur. The failure of controllers to regain contact with the spacecraft was traced to an error in the software uploaded on 29/30 August which had deactivated the attitude thrusters. This resulted in a loss of lock on the Sun, resulting in the spacecraft orienting the solar arrays away from the Sun, thus depleting the batteries. The spacecraft flew past Mars without activating its science instruments or deploying its lander.

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