GeoLITE (original) (raw)

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GeoLITE [NRO]

GeoLITE (Geosynchronous Lightweight Technology Experiment) was an advanced, experimental communications satellite featuring Laser and UHF communication devices. It is operated by the NRO.

GeoLITE was the first mission for TRW's T-310 satellite bus, a new lightweight, highly stable platform capable of a range of missions. TRW had system integration responsibility for GeoLITE, including the satellite development, integration and preparation for launch. Teammates included the Massachusetts Institute of Technology�s Lincoln Laboratory, which was responsible for the laser communications payload, and Hughes Space and Communications Company, which was responsible for the UHF communications payload

The laser communications experiments consisted of:

The UHF payload was part of the IBS-S (Integrated Broadcast Service - Simplex) inteligence data dissemination architecture to replace the older military satellite communications (MILSATCOM) archtecture. Other IBS-S payloads were flown on different missions to provide geostationary and polar coverage.

The satellite was designed and built in 3 1/2 years using streamlined program methodologies.

Note: The NROL designations refer to the launch, not to the payload.

Nation: USA
Type / Application: Communication (Experimental)
Operator: NRO
Contractors: TRW (prime); Massachusetts Institute of Technology�s Lincoln Laboratory (laser payload); Hughes (IBS-S payload)
Equipment: GLT, GLOM, IBS-S
Configuration: T310
Propulsion: TR-500 SCAT
Power: 2 deployable solar arrays, batteries
Lifetime: 9 years
Mass: ca. 1800 kg
Orbit: GEO
Satellite COSPAR Date LS Launch Vehicle Remarks
GeoLITE (USA 158, NROL 17) 2001-020A 18.05.2001 CC SLC-17B Delta-7925

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