Report discusses calculations of thermodynamic aspects of refilling tanks with cryogenic liquids in low or zero gravity. Calculations required to design prototype system resupplying cryogenic propellant liquids to re-usable spacecraft not returning to Earth. Equations and computer programs developed for thermodynamic analysis used to extrapolate important design information from orbiting small-scale versions of system.
Analysis Of Transfer Of Cryogens In Low Gravity
NASA Tech Briefs ; 17 , 7
1993-07-01
Sonstige
Keine Angabe
Englisch
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