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Other Designations: Global Low Orbiting Message Relay. Class: Communications. Type: Military. Nation: United States. Agency: DARPA. Manufacturer: Defense Systems Inc. (now CTA).
GLOMR was a DARPA mission designed to demonstrate the ability to read out, store, and forward data from remote ground-based sensors. The satellite was first scheduled for deployment from STS-51B, but a battery problem forced a return to Earth for repair. Reflown and deployed from STS-61A, the vehicle finally re-entered after 14 months. The total price was less than 1 million dollars. Spacecraft: Small, 62-sided polyhedron. Unstabilised. Design included redundant transmitters, receivers, batteries, and battery charge control systems. It had two CMOS microprocessors - one for communications control, the other for scheduling, mass memory, housekeeping, and mission control, telemetry, and command functions.
Design Life: 1 year . Maximum Diameter: 0.3 m.
30 October 1985
GLOMR; GLOMAR Launch Site: Cape Canaveral . Launch Vehicle: Shuttle. Mass: 52 kg. Perigee: 317 km. Apogee: 332 km. Inclination: 57.0 deg.
Released from STS 61A 11/1/85. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).
05 April 1990
USA 55 Launch Site: Edwards . Launch Vehicle: Pegasus. Mass: 25 kg. Perigee: 477 km. Apogee: 642 km. Inclination: 94.1 deg.
Store and forward.
- 2 - McDowell, Jonathan, The United Nations Registry of Space Objects, Harvard University, 1997. HTML when accessed: http://hea-www.harvard.edu/QEDT/jcm/space/un/un.html
- 6 - JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. HTML when accessed: http://msl.jpl.nasa.gov/home.html
- 279 - McDowell, Jonathan, Launch Log, October 1998. HTML when accessed: http://hea-www.harvard.edu/~jcm/space/log/launch.html
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Last update 12 March 2001.
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© Mark Wade, 2001 .