Possible weight saving from catalysis of recombination in hydrogen rockets.
Weight savings advantage of catalyzed hydrogen rocket propellant, discussing specific impulse and tankage volume
Engineering topics
Publications and source records attributed to Mates, R. E..
Weight savings advantage of catalyzed hydrogen rocket propellant, discussing specific impulse and tankage volume
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Nonequilibrium ionization in asymmetric plasma sheath determined for Apollo spacecraft at superorbital velocity reentry
Direct calculation method for supersonic inviscid flow around axisymmetric blunt body with conically reentrant afterbody flying at large angle of attack
Computer program for numerical solution of reacting gas mixture nonequilibrium expansions
Direct numerical method for calculation of supersonic inviscid flow about axisymmetric blunt body at large angle of attack
Oxygen and oxygen-nitrogen mixtures as catalysts for hydrogen atom recombination in rocket nozzles
Multiple temperature heat bath models described by classical thermodynamic temperatures for vibrational and chemical nonequilibrium processes
Nonequilibrium inviscid flow about arbitrarily shaped body with detached shock waves, using method with time derivative and bypassing boundary conditions
Temperature of classical thermodynamics in nonequilibrium processes