Introduction: The thermal energy balance of any space mission element, whether it is a spacecraft, a permanent and crewed lunar base, or a space suit, is derived as a function of heat released by personnel and/or components installed within the outer shell and heat received from the surrounding environment.
CITATION STYLE
Fraser, S. D. (2013). Theory and applications of cooling systems in lunar surface exploration. In Moon: Prospective Energy and Material Resources (Vol. 9783642279690, pp. 405–437). Springer-Verlag Berlin Heidelberg. https://doi.org/10.1007/978-3-642-27969-0_18
Mendeley helps you to discover research relevant for your work.