DocumentCode :
2553051
Title :
Spacecraft modular architecture design for on-orbit servicing
Author :
Reynerson, Charles M.
Author_Institution :
Ball Aerosp. & Technol. Corp., Boulder, CO, USA
Volume :
4
fYear :
2000
fDate :
2000
Firstpage :
227
Abstract :
The Spacecraft Modular Architecture Design (SMAD) Concept involves the use of an on-orbit servicing vehicle to replace and/or replenish components on a spacecraft. This study was conducted to evaluate the potential cost and benefits for on-orbit satellite servicing. Actual satellite data were used to estimate a baseline cost and to establish an operational design. This paper gives an overview of the study including the selection of servicing methodology, benefits of servicing, spacecraft impacts, selection of spacecraft components/subsystems to service, derived servicer requirements, servicer point design, and a costing evaluation
Keywords :
artificial satellites; cost-benefit analysis; life cycle costing; maintenance engineering; baseline cost; components selection; on-orbit servicing; operational design; potential cost-benefits; rendezvous docking; satellite servicing; servicer point design; servicer requirements; servicing methodology; servicing vehicle; spacecraft modular architecture design; Costing; Costs; History; Low earth orbit satellites; Orbital robotics; Payloads; Space shuttles; Space stations; Space technology; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
0-7803-5846-5
Type :
conf
DOI :
10.1109/AERO.2000.878426
Filename :
878426
Link To Document :
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