1. An advance in transfer line chilldown heat transfer of cryogenic propellants in microgravity using microfilm coating for enabling deep space exploration
- Author
-
Jason Hartwig, Jacob N. Chung, S.R. Darr, Jun Dong, and Hao Wang
- Subjects
Physics and Astronomy (miscellaneous) ,Physiology ,Materials Science (miscellaneous) ,Medicine (miscellaneous) ,engineering.material ,01 natural sciences ,Biochemistry, Genetics and Molecular Biology (miscellaneous) ,Article ,03 medical and health sciences ,Deep space missions ,Coating ,0103 physical sciences ,QP1-981 ,Aerospace engineering ,010306 general physics ,030304 developmental biology ,Propellant ,0303 health sciences ,Earth's orbit ,business.industry ,Transfer line ,Mars Exploration Program ,Agricultural and Biological Sciences (miscellaneous) ,Deep space exploration ,Space and Planetary Science ,Environmental chemistry ,Heat transfer ,Physics::Space Physics ,engineering ,Environmental science ,Astrophysics::Earth and Planetary Astrophysics ,business ,TP248.13-248.65 ,Biotechnology - Abstract
The extension of human space exploration from a low earth orbit to a high earth orbit, then to Moon, Mars, and possibly asteroids is NASA’s biggest challenge for the new millennium. Integral to this mission is the effective, sufficient, and reliable supply of cryogenic propellant fluids. Therefore, highly energy-efficient thermal-fluid management breakthrough concepts to conserve and minimize the cryogen consumption have become the focus of research and development, especially for the deep space mission to mars. Here we introduce such a concept and demonstrate its feasibility in parabolic flights under a simulated space microgravity condition. We show that by coating the inner surface of a cryogenic propellant transfer pipe with low-thermal conductivity microfilms, the quenching efficiency can be increased up to 176% over that of the traditional bare-surface pipe for the thermal management process of chilling down the transfer pipe. To put this into proper perspective, the much higher efficiency translates into a 65% savings in propellant consumption.
- Published
- 2021