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
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