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Weber

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Status: xRet. ??.12.2002. Number: 2 . Duration: 18.77 days. Location: Utah.

The Weber State Center for Aerospace Technology began development of a low-cost satellite bus for low earth orbit applications and also operated the ground control facility.

• NUSAT-1 - . Payload: Challenger F7 / Nusat / GLOMR [1]. Mass: 52 kg (114 lb). Nation: USA. Agency: Weber. Class: Surveillance. Type: Radar calibration target. Spacecraft: NUSAT. Decay Date: 1986-12-15 . USAF Sat Cat: 15666 . COSPAR: 1985-034B. Apogee: 354 km (219 mi). Perigee: 345 km (214 mi). Inclination: 57.00 deg. Period: 91.50 min. Air traffic control radar calibration. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .

• Oscar 18 - . Payload: Webersat. Mass: 12 kg (26 lb). Nation: USA. Agency: Weber. Program: Oscar. Class: Communications. Type: Amateur radio communications satellite. Spacecraft: Oscar. USAF Sat Cat: 20441 . COSPAR: 1990-005F. Apogee: 797 km (495 mi). Perigee: 780 km (480 mi). Inclination: 98.60 deg. Period: 100.60 min. Carried Earth imaging camera. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

• JAWSAT - . Payload: P98-1. Mass: 64 kg (141 lb). Nation: USA. Agency: USAF AFMC. Manufacturer: Weber. Class: Technology. Type: Navigation technology satellite. Spacecraft: JAWSAT. USAF Sat Cat: 26061 . COSPAR: 2000-004A. Apogee: 805 km (501 mi). Perigee: 753 km (468 mi). Inclination: 100.20 deg. Period: 100.36 min. Joint USAF Academy/Weber State Satellite. Payloads included a plasma experiment, a particle detector, and a technology test..