The ALEXIS mission recovery

Conference · Tue Mar 01 00:00:00 EST 1994

OSTI ID:142518

Bloch, J; Armstrong, T; Dingler, B; Enemark, D; Holden, D; Little, C; Munson, C; Priedhorsky, B; Roussel-Dupre, D; Smith, B ^[1]; Warner, R; Dill, B; Huffman, G; McLoughlin, F; Mills, R; Miller, R ^[2]

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1. Los Alamos National Lab., NM (United States)
2. AeroAstro, Inc., Herndon, VA (United States)

The authors report the recovery of the ALEXIS small satellite mission. ALEXIS is a 113-kg satellite that carries an ultrasoft x-ray telescope array and a high-speed VHF receiver/digitizer (BLACKBEARD), supported by a miniature spacecraft bus. It was launched by a Pegasus booster on 1993 April 25, but a solar paddle was damaged during powered flight. Initial attempts to contact ALEXIS were unsuccessful. The satellite finally responded in June, and was soon brought under control. Because the magnetometer had failed, the rescue required the development of new attitude control-techniques. The telemetry system has performed nominally. They discuss the procedures used to recover the ALEXIS mission.

• Research Organization: Los Alamos National Lab. (LANL), Los Alamos, NM (United States)
• Sponsoring Organization: USDOE, Washington, DC (United States)
• DOE Contract Number: W-7405-ENG-36
• OSTI ID: 142518
• Report Number(s): LA-UR-94-503; CONF-940259-1; ON: DE94007549; TRN: AHC29407%%50
• Resource Relation: Conference: 17. annual American Astronomical Society (AAS) guidance and control conference, Keystone, CO (United States), 2-6 Feb 1994; Other Information: PBD: 1994
• Country of Publication: United States
• Language: English

Related Subjects

14 SOLAR ENERGY
42 ENGINEERING NOT INCLUDED IN OTHER CATEGORIES
SATELLITES
PHOTOVOLTAIC POWER SUPPLIES
ELECTRONIC GUIDANCE
NAVIGATION
ATTITUDE CONTROL