NASA NTRS · 19680024607
Propellant selection for spacecraft propulsion systems. Volume 3 - Thermodynamics and propulsion Final report
Abstract
Thermodynamic analysis of spacecraft thermal control and pressurization requirements for Mars Orbiter and Mars Excursion Module missions
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1968-08-30. Propellant selection for spacecraft propulsion systems. Volume 3 - Thermodynamics and propulsion Final report. https://ntrs.nasa.gov/citations/19680024607
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