Design and verification of the SAX satellite

Details Design and verification of the SAX satellite Design and verification of the SAX satellite

Oct 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993graz.iafct....f&link_type=abstract

IAF, International Astronautical Congress, 44th, Graz, Austria, Oct. 16-22, 1993, 16 p.

Astronomy and Astrophysics

Astronomy

Scintillation Counters, Spacecraft Design, Spacecraft Power Supplies, X Ray Astronomy, X Ray Imagery, X Ray Sources, Mission Planning, Satellite Attitude Control, Service Life

Scientific paper

The paper describes the design concept of the Satellite for Astronomy in X-rays (SAX), together with the mission characteristics and operational concept. Particular attention is given to the SAX satellite configuration (including the data management and communication system, the SAX electrical power system architecture, the attitude control computer, and the star tracker) and the SAX payload. Also discussed are the major system data and requirements, the system level verification process, the payload verification, and the payload technological features. The SAX launch is planned at the end of 1995, for a minimum operational life of two years.

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