Data were computed assuming equilibrium composition during isentropic expansion using normal hydrogen as propellant for chamber pressures from 0.146960 to 1469.60 psia, pressure ratios from 1 to 3000, and chamber temperatures from 600 to 5000 K; performance parameters are given.
Compilation of thermodynamic properties, transport properties, and theoretical rocket performance of gaseous hydrogen
NASA -- Tech Note
1960
71 pages
Article (Journal)
English
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