Hughes (original) (raw)

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Hughes

American manufacturer of rockets, spacecraft, and rocket engines. Hughes Aircraft Co., USA

AKA: Hughes Aircraft Co;Hughes Tool Co.

People: Rosen, Harold, Jarvis, Cunningham, Stephen, Konrad. Country: USA. Engines: Sert-I Cesium, SEPST, SIT- 5, SEPS, P78-2, XIPS-25 1.3 kW, XIPS-25 4.2 kW, IAPS, LR107, XIPS-13 0.44 kW. Spacecraft: Intelsat 1, Intelsat 2, ATS-1, ATS-2, ATS-3, ATS-4, TACSAT, ATS-5, Intelsat 4, HS 333, Intelsat 4A, Pioneer 12, Pioneer 13, HS 376, HS 381, HS 393, HS 601, Milstar, HS 376W, Orbview-2, CAPRICORN, HS 702. Launch Vehicles: Jarvis launch vehicle. Stages: Falcon engine. Agency: Aussat.

1992 December 21 - . 11:21 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: Chang Zheng 2E. FAILURE: Shortcomings in the guidance system lead to the vehicle not anticipating the true effects of horizontal wind-shear once the mountains surrounding the launch site were cleared. This caused the nose fairing to collapse 45 seconds after launch.. Failed Stage: G.

Aussat B2 / Optus B2 - . Payload: Optus B2 / Star 63F. Mass: 2,760 kg (6,080 lb). Nation: Australia. Agency: Hughes. Program: Aussat. Class: Communications. Type: Military communications satellite. Spacecraft: HS 601. Decay Date: 1995-06-29 . USAF Sat Cat: 22278 . COSPAR: 1992-090A. Apogee: 816 km (507 mi). Perigee: 206 km (128 mi). Inclination: 28.10 deg. Period: 94.90 min. Despite collapse of the nose fairing and near-desctruction of the payload, the launch vehicle continued on to place the wreckage of Optus-B2, and the Star-63F Kick-Motor into low earth orbit..

2000 March 12 - . 14:49 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: Odyssey. LV Family: Zenit. Launch Vehicle: Zenit-3SL. FAILURE: Second stage shut down prematurely due to a valve software command mistake. The satellite fell in the South Pacific, south of Pitcairn Island.. Failed Stage: 2.

ICO F-1 - . Mass: 2,750 kg (6,060 lb). Nation: USA. Agency: ICO. Manufacturer: Hughes. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 601. Apogee: 200 km (120 mi). First ICO Global Communications satellite. Lost due to launch vehicle failure; was to have entered a 10,300 km x 45 deg circular orbit. ICO's satellites would carry multiple spot beams for mobile communications..

2007 August 14 - . 23:44 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA.

Spaceway 3 - . Mass: 6,075 kg (13,393 lb). Nation: USA. Agency: Hughes. Manufacturer: El Segundo. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 702. USAF Sat Cat: 32018 . COSPAR: 2007-036A. Apogee: 35,788 km (22,237 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.0200 deg. Period: 1,436.12 min. Satellite launched for Hughes Network Systems, with a Ka-band payload for space-based internet. Mass 3655 kg dry..

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