American technology satellite. One launch, 1994.03.13, USA 102. GPS receiver and data processor technology tests.
Gross mass: 203 kg (447 lb).
More... - Chronology...
First Launch: 1994.03.13.
Number: 1 .
Taurus Pad-launched launch vehicle using Pegasus upper stages and Castor-120 first stage. More...
Associated Launch Vehicles
ARPA Taurus American all-solid orbital launch vehicle. Four stage version consisting of 1 x TU-904 + 1 x Orion 50 + 1 x Orion 50 + 1 x Orion 38 More...
Taurus American all-solid orbital launch vehicle. Pad-launched launch vehicle using Pegasus upper stages and Castor-120 first stage. First launch used slightly larger Peacekeeper ICBM first stage instead of Castor-120. Under a 2002 contract from Boeing, Orbital developed a three-stage version of Taurus to serve as the interceptor boost vehicles for the US government's missile intercept system. The firm portion of the company's contract, awarded in early 2002, was valued at $450 million and extended through 2007. More...
Associated Manufacturers and Agencies
USAF American agency overseeing development of rockets and spacecraft. United States Air Force, USA. More...
McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: here.
McDowell, Jonathan, Launch Log, October 1998. Web Address when accessed: here.
Associated Launch Sites
Vandenberg Vandenberg Air Force Base is located on the Central Coast of California about 240 km northwest of Los Angeles. It is used for launches of unmanned government and commercial satellites into polar orbit and intercontinental ballistic missile test launches toward the Kwajalein Atoll. More...
1994 March 13 -
22:32 GMT - .
. Launch Complex
: Vandenberg 576E
. LV Family
. Launch Vehicle
: ARPA Taurus
. LV Configuration
: ARPA Taurus T1 1110.
- USA 102 - .
Payload: DarpaSat. Mass: 203 kg (447 lb). Nation: USA. Agency: DARPA. Class: Technology. Type: Navigation technology satellite. Spacecraft: DARPASAT. USAF Sat Cat: 23031 . COSPAR: 1994-017B. Apogee: 556 km (345 mi). Perigee: 532 km (330 mi). Inclination: 105.0000 deg. Period: 95.50 min. Summary: GPS receiver and data processor technology tests. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B)..
Home - Browse - Contact
© / Conditions for Use