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SEDS
SEDS 1
SEDS 1
Credit: Manufacturer Image
Students for the Exploration and Development of Space, USA. Built tether technology satellite. Technology satellite operated by NASA, USA. Launched 1993 - 1994.

AKA: Small Expendable-tether Deployer System.. Status: Operational 1993. First Launch: 1993-03-30. Last Launch: 1994-03-10. Number: 4 . Gross mass: 25 kg (55 lb).


More at: SEDS.

Family: Technology, Tether technology satellite. Country: USA. Spacecraft: SEDSAT. Launch Vehicles: Thor, Delta, Delta 2 7000, Delta 7925. Projects: Navstar, STS. Launch Sites: Cape Canaveral, Cape Canaveral LC17A. Agency: USAF. Bibliography: 2, 279, 6, 6861.

1993 March 30 - . 03:09 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Delta 7925.
  • SEDS 1 Deployer - . Payload: SEDS 1 Deployer. Mass: 25 kg (55 lb). Nation: USA. Agency: MDAC. Program: Navstar. Spacecraft: SEDS. Decay Date: 1999-05-05 . USAF Sat Cat: 22583 . COSPAR: 1993-017C. Apogee: 1,292 km (802 mi). Perigee: 305 km (189 mi). Inclination: 36.1000 deg. Period: 100.84 min.
  • SEDS 1 - . Payload: SEDS 1 End Mass/Tether. Mass: 25 kg (55 lb). Nation: USA. Agency: NASA Huntsville. Class: Technology. Type: Tether technology satellite. Spacecraft: SEDS. Decay Date: 1993-03-30 . USAF Sat Cat: 22582 . COSPAR: 1993-017B. Apogee: 719 km (446 mi). Perigee: 183 km (113 mi). Inclination: 36.0000 deg. Period: 93.62 min. Small Expendable-tether Deployer System. .

1994 March 10 - . 03:40 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Delta 7925.
  • SEDS 2 - . Payload: SEDS 2 End Mass. Mass: 25 kg (55 lb). Nation: USA. Agency: MDSSC. Program: Navstar. Spacecraft: SEDS. COSPAR: 1994-016xx.
  • SEDS 2 Deployer - . Payload: SEDS 2 Deployer. Mass: 25 kg (55 lb). Nation: USA. Agency: MDAC. Program: Navstar. Spacecraft: SEDS. Decay Date: 1994-05-08 . USAF Sat Cat: 23028 . COSPAR: 1994-016B. Apogee: 341 km (211 mi). Perigee: 340 km (210 mi). Inclination: 32.3000 deg. Period: 91.34 min.

1998 October 24 - . 12:08 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. Launch Pad: SLC17A. LV Family: Thor. Launch Vehicle: Delta 7326-9.5.
  • SEDSAT 1 - . Nation: USA. Agency: Boeing. Manufacturer: SEDS. Program: STS. Class: Technology. Type: Navigation technology satellite. Spacecraft: SEDSAT. USAF Sat Cat: 25509 . COSPAR: 1998-061B. Apogee: 1,050 km (650 mi). Perigee: 544 km (338 mi). Inclination: 31.4000 deg. Period: 100.80 min.

    Following separation of the third stage and the primary Deep Space 1 payload, the Delta second stage manoeuvred from its 185 km parking orbit to a 174 km x 2744 km x 28.5 degree orbit. It then released the SEDSAT micro-satellite, built by the Huntsville, Alabama chapter of SEDS (the Students for the Exploration and Development of Space). SEDSAT has two amateur radio transponders and an earth imaging camera.



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