A study of learning curve impact on three identical small spacecraft

IEEE Aerospace Conference Proceedings

Volumn 6, Issue , 2004, Pages 3970-3975

  Chen, Guangming ^a   McLennan, Douglas D ^b  

^a Center of Excellence for Tactical and Advanced Communications Technologies   (United States)

^b NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

GODDARD SPACE FLIGHT CENTER; LAUNCH READINESS DATE (LRD); MULTIPLE-SPACECRAFT PRODUCTION MISSION; ROBUST DESIGN;

ELECTRIC POWER SYSTEMS; LEARNING SYSTEMS; PROJECT MANAGEMENT; RISK MANAGEMENT; ROBUSTNESS (CONTROL SYSTEMS); SATELLITES;

SPACECRAFT;

EID: 11244255174     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.2004.1368215     Document Type: Conference Paper

References (7)

1. Evans, B. (editor): Satellite Communication Systems, 3rd edition, Institution of Electrical Engineers, London, UK, 1999
2. Bertheux, P., Douillet, F. and Chiarini, J. C.: A low-cost multi-mission bus for small satellite applications, Space Technology, Vol 18, pp. 171-174, 1998
3. NASA Goddard Space Flight Center, Concept Study Report for the New Millennium Space Technology 5 Small Satellite Constellation Theme, Goddard Space Flight Center, July 15, 1999.
4. rd edn, Microcosm Press and Kluwer Academic Publishers, 1999.
5. th edn., West Publishing Company, 1993
6. Modern Technologies Corporation: Defense Manufacturing Management - Guide for Program Managers, Defense Systems Management College, Fort Belvoir, VA, April 1989.
7. Chen, G. and Oberright, J., "Integrating Robustness into ST-5 Nano-Satellite Development for Inexpensive Space Missions", an article in Smaller Satellites: Bigger Business? Space Studies Vol. 6 (edited by M. Rycroft and N. Crosby), Kluwer Academic Publishers, 2002.