Cryopumping Rocket Exhaust Products at High Throughputs and Low Pressure
Preliminary analyses for the design of a cryopumping system to freeze out large-mass flow rates of rocket exhaust products are presented in this report. The controlling design factors, results of preliminary analysis, and test data to show feasibility, are included.
KeywordsHeat Exchanger Knudsen Number Space Simulation Plate Spacing Exhaust Product
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- 1.B.M. Bailey and R.L. Chuan, “Gryopuinpingfor High Vacuum with Low Power,” Fifth. National Symposium on Vacuum Technology Transactions, American Vacuum Society, Pergaraon Press, New York (1958), p. 262.Google Scholar