Development of MINISAT 01 Scientific Payload

Details Development of MINISAT 01 Scientific Payload Development of MINISAT 01 Scientific Payload

Mar 2001

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2001ap%26ss.276...21t&link_type=abstract

Astrophysics and Space Science, v. 276, Issue 1, p. 21-29 (2001).

Astronomy and Astrophysics

Astrophysics

Scientific paper

The MINISAT design is a modular concept, and accordingly the Scientific Payload of Mission 01 is a self-contained Payload Module (PLM). This philosophy offers the advantage that the Payload and the Platform may be assembled independently and coupled together at a later stage. The mechanical, thermal, power and data interfaces have to be secured along the design and development phases. The MINISAT 01 PLM with three instruments, EURD, LEGRI and CPLM, integrates on a structural tray a dozen of equipment supplied by more than ten participant Institutions. The Assembly, Integration and Verifications (AIV) of the PLM, was performed at INTA, providing the common structural, harnessing and thermal control subsystems. In this paper an overview is presented of the PLM layout of the different models and the qualification and acceptance testing.

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