Spacecraft thermal analysis and control by thermal energy optimum distribution

Journal of Spacecraft and Rockets

Volumn 39, Issue 1, 2002, Pages 149-152

  Fragnito, Marino ^a   Pastena, Massimiliano ^b   D’errico, Marco ^b  

^a Grp d'Etudes/de Conseils Ingenierie   (France)

^b SECOND UNIVERSITY OF NAPLES   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; COMPUTER SOFTWARE; ELECTRIC POWER GENERATION; FINITE ELEMENT METHOD; LAUNCHING; MATHEMATICAL MODELS; ORBITS; REMOTE SENSING; THERMOANALYSIS;

MICROSATELLITES;

SPACECRAFT;

EID: 0036198882     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3794     Document Type: Article

References (5)

1. A bistatic SAR mission for earth observation based on a small satellite
2. Design of smart microsatellite deployable solar wings
3. SMART microsatellite structure, mechanisms and thermal design