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GeoLITE is an advanced
technology demonstration satellite with a laser communications
experiment and an operational UHF communications mission. The
GeoLITE program also employs streamlined acquisition and
design-to-cost methodologies to complete the satellite
development, integration and launch. The satellite is based on a
modular bus design with multi-mission capabilities.
The
satellite was designed and built in 3 1/2 years using streamlined
program methodologies by TRW Space & Electronics, Redondo
Beach, a subsidiary of TRW, Inc. for the National Reconnaissance
Office (NRO). Laser technology that might provide future spy
satellites with a better way to transmit information to Earth will
be tested from its position in geosynchronous orbit over the
Indian Ocean. GeoLITE will also serve as an operational
telecommunications satellite for the NRO using a conventional UHF
communications package. Additional details of how the system will
work, including location of ground stations and the orbital
position of GeoLITE, remain classified.
The 635 kg (1400
lbm) satellite GeoLITE (Geosynchronous Lightweight Technology
Experiment), an advanced technology demonstration satellite, is
the first mission for TRW's T-310 satellite bus, a new
lightweight, highly stable platform capable of a range of missions.
TRW has system integration responsibility for GeoLITE, including
the satellite development, integration and preparation for launch.
The contract award was announced on July 10, 1998.
The US$77.8 million contract nearly doubled in cost to
US$130 million, not including launch costs. Launch costs were not
released by the NRO.
The T-310 bus is
built of lightweight composite materials that allow for increased
instrument weight and reduced launch costs. The T-310 modular bus
design provides flexible capability for a variety of applications,
including geostationary communications and weather observation
missions, as well as planetary missions. The design features
common subsystems scalable to the mission-specific needs.
Instrument payloads can be attached on a “mix and match” basis
without changes in the overall design or subsystem support
requirements. The GeoLITE mission is expected to last nine years.
The bus provides 1.2 kW EOL (End of Life) electric power. The
satellite is based on previous TRW spacecraft designs, including
NASA's Total Ozone Mapping Spectrometer Earth Probe (TOMS) and
China's ROCSAT-1 satellite.
The
Massachusetts Institute of Technology's Lincoln Laboratory was
responsible for developing for the laser communications payload.
The conventional ultra-high frequency (UHF) communications relay
package was built by Boeing Satellite Systems.
GeoLITE
Geosynchronous
Lightweight
Technology
Experiment
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SPACECRAFT
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| Int'l Designation |
2001-020A
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Launched
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| Owner / Sponsor |
U.S.
National Reconnaissance Office (NRO)
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| Mission |
Technology
Demonstrator - Military Communications
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| Manufacturer / Model |
TRW
Space & Electronics
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T-310
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| Launch Mass |
635
kg (1400 lbm)
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| Dimensions |
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| Mission Orbit |
GSO
|
Indian Ocean
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| Design Life |
9
years
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| Power (EOL) |
1.2
kW
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LAUNCH
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| Launch Vehicle
Model |
Delta
II 7925 |
| Date / Time (UTC) |
2001
May 18
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17:45
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FINANCIAL
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| Satellite cost |
US$130
million
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| Web Links |
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