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Some operational aspects of a rotating advanced-technology space station for the year 2025The study of an Advanced Technology Space Station which would utilize the capabilities of subsystems projected for the time frame of the years 2000 to 2025 is discussed. The study includes tradeoffs of nuclear versus solar dynamic power systems that produce power outputs of 2.5 megawatts and analyses of the dynamics of the spacecraft of which portions are rotated for artificial gravity. The design considerations for the support of a manned Mars mission from low Earth orbit are addressed. The studies extend to on-board manufacturing, internal gas composition effects, and locomotion and material transfer under artificial gravity forces. The report concludes with an assessment of technology requirements for the Advanced Technology Space Station.
Document ID
19880017013
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Queijo, M. J.
(Bionetics Corp. Hampton, VA, United States)
Butterfield, A. J.
(Bionetics Corp. Hampton, VA, United States)
Cuddihy, W. F.
(Bionetics Corp. Hampton, VA, United States)
King, C. B.
(Bionetics Corp. Hampton, VA, United States)
Stone, R. W.
(Bionetics Corp. Hampton, VA, United States)
Wrobel, J. R.
(Bionetics Corp. Hampton, VA, United States)
Garn, P. A.
(Bionetics Corp. Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-181617
NAS 1.26:181617
Report Number: NASA-CR-181617
Report Number: NAS 1.26:181617
Accession Number
88N26397
Funding Number(s)
PROJECT: RTOP 506-49-31-01
CONTRACT_GRANT: NAS1-18267
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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