Heat transfer characteristics of liquid hydrogen as a coolant for the LO2/LH2 rocket thrust chamber with the channel wall construction
Author:
Affiliation:
1. National Aerospace Laboratory, Ohgawara, Miyagi, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-1107
Reference15 articles.
1. M.Niino etal, Heat Transfer Japanese Research, 9-2 (1980-41, 61.
2. K.K.Huze 1 et al., NASA SP-125, (19711, 81.
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