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GLOMR
GLOMR Credit: Manufacturer Image |
American military store-dump communications satellite. Experimental communication satellite built by DSI, Rockwell for DARPA, USAF STP (Space Test Program), USA. Launched 1985. Used GLOMR Bus (62-sided polyhedron, unstabilized, body mounted solar cells).
AKA: SECS. Status: Operational 1985. First Launch: 1985-04-29. Last Launch: 1990-04-05. Number: 3 . Gross mass: 52 kg (114 lb). Height: 0.60 m (1.96 ft).
GLOMR (Global Low Orbiting Message Relay) was a DARPA project 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. The spacecraft was a small, 62-sided polyhedron, and unstabilized. The 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.
The SECS (Special Experimental Communications System) or GLOMR 2 was an improved digital store and forward communications spacecraft for a classified mission. The design was similar to GLOMR with more data storage, greater redundancy, and more space qualified hardware content. SECS was the first spacecraft launched on the air-launched Pegasus launch vehicle. The spacecraft operated for 3.5 years. The spacecraft had a spherical structure, and was unstabilized with body mounted solar cells. The payload was to GLOMR.
More at: GLOMR.
Subtopics
Family:
Communications,
Military store-dump comsat.
Country:
USA.
Launch Vehicles:
Space Shuttle,
Pegasus.
Launch Sites:
Cape Canaveral,
Cape Canaveral LC39A,
Point Arguello WADZ.
Agency:
USN,
DARPA,
CTA Space Systems.
Bibliography:
2,
279,
6.
Photo Gallery
| Pegsat Credit: Manufacturer Image |
1985 April 29 - .
16:02 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
Launch Platform: MLP2.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- GLOMR - .
Nation: USA.
Agency: NASA.
Program: STS.
Spacecraft: GLOMR.
Decay Date: 1985-05-06 . USAF Sat Cat: 15665 . COSPAR: 1985-034xx. Apogee: 359 km (223 mi). Perigee: 346 km (214 mi). Inclination: 57.00 deg. Period: 91.60 min.
1985 October 30 - .
17:00 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC39A.
Launch Platform: MLP1.
LV Family:
Shuttle.
Launch Vehicle:
Space Shuttle.
- GLOMR; GLOMAR - .
Payload: Challenger F9 / GLOMR 1. Mass: 52 kg (114 lb). Nation: USA.
Agency: USN.
Class: Communications.
Type: Military communications satellite. Spacecraft: GLOMR.
Decay Date: 1986-12-26 . USAF Sat Cat: 16231 . COSPAR: 1985-104B. Apogee: 332 km (206 mi). Perigee: 317 km (196 mi). Inclination: 57.00 deg. Period: 91.00 min. Released from STS 61A 11/1/85. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B)..
1990 April 5 - .
19:10 GMT - .
Launch Site:
Point Arguello.
Launch Complex:
Point Arguello WADZ.
Launch Pad: Aircraft from Edwards..
Launch Platform: NB-52 008.
Launch Vehicle:
Pegasus.
- USA 55 - .
Payload: GLOMR 2 / TERCEL / SECS. Mass: 25 kg (55 lb). Nation: USA.
Agency: DARPA.
Class: Communications.
Type: Military communications satellite. Spacecraft: GLOMR.
USAF Sat Cat: 20547 . COSPAR: 1990-028B. Apogee: 642 km (398 mi). Perigee: 477 km (296 mi). Inclination: 94.10 deg. Period: 95.90 min. Store and forward. Air dropped in Point Arguello WADZ..
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