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A compilation of lunar and Mars exploration strategies utilizing indigenous propellantsThe use of propellants manufactured from indigenous space materials has the potential to significantly reduce the amount of mass required to be launched from the Earth's surface. The extent of the leverage, however, along with the cost for developing the infrastructure necessary to support such a process, is unclear. Many mission analyses have been performed that have attempted to quantify the potential benefits of in situ propellant utilization. Because the planning of future space missions includes many unknowns, the presentation of any single study on the use of in situ propellants is often met with critics' claims of the inaccuracy of assumptions or omission of infrastructure requirements. The results of many such mission analyses are presented in one format. Each summarized mission analysis used different assumptions and baseline mission scenarios. The conclusion from the studies is that the use of in situ produced propellants will provide significant reductions in Earth launch requirements. This result is consistent among all of the analyses regardless of the assumptions used to obtain the quantitative results. The determination of the best propellant combination and the amount of savings will become clearer and more apparent as the technology work progresses.
Document ID
19920010595
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Linne, Diane L.
(NASA Lewis Research Center Cleveland, OH, United States)
Meyer, Michael L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Propellants And Fuels
Report/Patent Number
E-6790
NASA-TM-105262
NAS 1.15:105262
Accession Number
92N19837
Funding Number(s)
PROJECT: RTOP 506-42-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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