Design of smart microsatellite deployable solar wings

Acta Astronautica

Volumn 46, Issue 2, 2000, Pages 335-344

  Fragnito, Marino ^a   Pastena, Massimiliano ^b  

^a SECOND UNIVERSITY OF NAPLES   (Italy)

^b UNIVERSITY OF NAPLES FEDERICO II   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

CARBON FIBER REINFORCED PLASTICS; COMPUTER SIMULATION; COMPUTER SOFTWARE; DESIGN; HONEYCOMB STRUCTURES; ORBITS; SOLAR EQUIPMENT; TEMPERATURE CONTROL; WINGS;

ALUMINUM HONEYCOMB CORE; DEPLOYABLE SOLAR WINGS; MASS TO EXPOSED SURFACE RATIO; MICROSATELLITE; THERMAL STRUCTURAL PROPERTIES;

SATELLITES;

EID: 0033897622     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(99)00228-3     Document Type: Article

References (11)

1. th Congress of the International Astronautical Federation, Turin, Italy (paper IAF-97-B.3.01), October 6-10 (1997).
2. th Congress of the International Astronautical Federation, Melbourne, Australia (paper IAF-98-R.1.06), September 28-October 2 (1998).
3. Ariane 4 - A.S.A.P. User's Manual. Issue 2 - Rev. 1 (1993)
4. Dow Corning Europe, Brussels, Belgium. Silicon Elastomer 93-500, Data Sheet number: 10-1062-01.
5. Amoco carbon fiber properties, Technical Information. Amoco Performance Products, Inc. USA.
6. Hexcel corp. - Satellite products. Product Technical Information. Document HSP98-2, (3/98).
7. ESA PSS 03 - 203, Structural Materials Handbook Vol. I: Polymer Composites.
8. David G. Gilmore, Satellite Thermal Control Handbook, The Aerospace Corporation Press, El Segundo, California (1994).
9. W. Larson and J. Wertz, Space Mission Analysis and Design, Kluwer Academy Publishers, The Netherlands (1992).
10. th Aerospace Mechanisms Symposium, Hampton, Virginia, May 15-17, (1996).
11. Peter. L. Conley, Space Vehicle Mechanism, John Wiley & Sons, Inc. New York NY (1998).