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Other Designations: Cosmic Background Explorer. Class: Astronomy. Type: Infrared. Destination: Sun Synchronous Orbit. Nation: USA. Agency: NASA. Manufacturer: NASA Goddard, Ball. The Cosmic Background Explorer's observations of diffuse cosmic background radiation helped answer basic questions such as whether the matter in the universe was homogeneously distributed, whether the universe was uniformly expanding and rotating, and how and when stars and galaxies first formed. COBE also mapped interstellar and interplanetary dust clouds. Originally planned for launch on the Shuttle, COBE was redesigned for launch aboard a Delta 2 following the Challenger disaster. COBE's supply of liquid helium was exhausted in September 1990, causing loss of the FIRAS instrument. The spacecraft was spin stabilized (0.8 rpm about sunline) using 3 reaction wheels and torque rods. Attitude control knowledge (4 arcmin) was provided by magnetometers, earth sensors, sun sensors, gyros. The satellite consisted of a hexagonal spacecraft bus and a cryostat containing 95.7 kg of liquid helium for cooling sensors. This was protected against solar and terrestrial radiation by a conical shield. Deployable solar panels provided 1050W BOL. Downlink was through the TDRSS relay satellite. The instrument payload consisted of the Differential Microwave Radiometer (DMR) to check the thermal and structural uniformity of the early universe, the Far Infrared Absolute Spectrometer (FIRAS) and the Diffuse IR Background Experiment (DIRBE), to search for the remnant radiation emitted from the primordial galaxies as they formed. Design Life: 1 year. Typical orbit: 887 x 898 km, incl. = 99.0 degree, sun synchronous. Length: 5.49 m (18.01 ft). Maximum Diameter: 2.44 m (8.00 ft). Mass: 2,265 kg (4,993 lb). COBE Chronology
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