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Transformers for Lunar Extreme Environments: Ensuring Long-Term Operations in Regions of Darkness and Low Temperatures: II - PhaseThis report shows how solar power could enable robotic operations in permanently shaded regions at lunar poles, to extract water ice and further produce liquid hydrogen and oxygen (LH2/LO2) propellant. The power needs are derived from an Architecture for Human Exploration of Mars based entirely on lunar propellant. The extraction of 10 metric tons of water per day (at 10% water in regolith) requires approx. 0.6 MW thermal power. Additional approx. 2 MW electric power are required to produce 7.5 metric tons of LH2/LO2 propellant per day, as needed by the architecture. To provide power to processing equipment inside Shackleton Crater, optimal locations are determined on the crater rim, from which several reflecting TransFormers (TFs) would redirect sunlight, achieving a combined period of illumination of approx. 99% of the year. A single 40-m diameter reflector could provide up to 1 MW solar power. Inflatable rigidizable tower support structures raise reflectors above ground for better solar exposure. There are trade-offs: e.g., two reflectors at ground level would provide the same combined total illumination as a single tower approx. 100-m tall. Such a TF based on a 100-m tower made with inflatable 2-m beams and 40-m diameter reflectors would be of similar dimensions as an MSL-class rover (approx. 1000 kg, 10 m(exp 3)). A TF-prospector rover combo could be designed and deployed in a Discovery-class mission searching for water. The TransFormers would be nodes of a Lunar Utilities Infrastructure that provides solar power year-round in the proximity of the pole, as well as local data transmission andintermittent direct to earth communications. This infrastructure would be instrumental infacilitating the development of a lunar economy.
Document ID
20180007435
Acquisition Source
Headquarters
Document Type
Other
Authors
Stoica, Adrian
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wilcox, Brian
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Alkalai, Leon
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ingham, Michel
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Quadrelli, Marco
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Salazar, Robert
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mantovani, Jim
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Henrickson, Jim
(Texas A&M Univ. College Station, TX, United States)
Valasek, John
(Texas A&M Univ. College Station, TX, United States)
Sercel, Joel
(TransAstra Corp. Lake View Terrace, CA, United States)
Date Acquired
November 1, 2018
Publication Date
November 1, 2017
Subject Category
Lunar And Planetary Science And Exploration
Energy Production And Conversion
Report/Patent Number
HQ-E-DAA-TN58829
Report Number: HQ-E-DAA-TN58829
Funding Number(s)
CONTRACT_GRANT: NNN12AA01C
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
fuel
propellant
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