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ATS-2
Credit - NASA
Other Designations: Applications Technology Satellite. Class: Technology. Type: Communications. Destination: Geosynchronous Orbit. Nation: USA. Agency: NASA, NSF. Manufacturer: Hughes.

ATS-2 was placed into an undesirable orbit due to a launch vehicle failure. Atmospheric torques in this orbit overcame the satellite's gravity gradient stabilization system, and caused a slow tumble. Although the satellite remained functional, the satellite was deactivated after six months due to the limited amount of data that could be received from the spacecraft. Spacecraft: Aluminum structure, drum solar array providing 125W BOL, 2 6 Ah NiCd batteries, gravity gradient stabilization. Payload: Meteorological experiments, C-band communications package

Design Life: 3 years. Typical orbit: Agena failure; 185 x 11177 km transfer orbit. Length: 1.80 m (5.90 ft). Maximum Diameter: 1.40 m (4.50 ft). Mass: 370 kg (810 lb).


ATS-2 Chronology
  • 1967 April 6 - ATS 2 - Program: ATS. Launch Site: Cape Canaveral. Launch Complex: LC12. Launch Vehicle: Atlas. FAILURE: Partial Failure. Mass: 370 kg (810 lb). Perigee: 177 km (109 mi). Apogee: 11,119 km (6,909 mi). Inclination: 28.40 deg. Period: 218.80 min.
    Launch vehicle failure left in useless orbit; communications tests.


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