DocumentCode
3207780
Title
Developing an efficient Space System Rapid Design Center
Author
Reynerson, Charles M.
Author_Institution
Ball Aerosp. & Technol. Corp., Boulder, CO, USA
Volume
7
fYear
2001
fDate
2001
Firstpage
7
Abstract
A Space System Rapid Design Center (RDC) can be used in quickly sizing and estimating the cost of space systems. Given candidate mission requirements for a satellite or constellation, clean-sheet of paper designs can be formulated resulting in the definition of key system parameters, such as size, power, weight, and payload performance. Rough cost models (Unmanned Spacecraft Cost Model - USCM, Small Satellite Cost Model - SSCM) can be linked to this to assist in determining Life Cycle Cost estimates. Existing spacecraft buses can be compared to the clean-sheet of paper design to determine their suitability for a particular mission. Higher fidelity tools can be used to link the spacecraft design to the mission data to assess impacts on mission effectiveness. Comparing the capabilities of a RDC to that of traditional aerospace concept design team processes, vehicle designs and performance information can be produced with a fraction of the resources and in much less time
Keywords
design engineering; life cycle costing; space vehicles; Space System Rapid Design Center; aerospace design; life cycle costing; small satellite cost model; spacecraft design; unmanned spacecraft cost model; vehicle design; Aerospace industry; Costs; Government; Payloads; Power system modeling; Process design; Proposals; Satellites; Space technology; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2001, IEEE Proceedings.
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-6599-2
Type
conf
DOI
10.1109/AERO.2001.931429
Filename
931429
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