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Influence of Combustion-chamber Length on Afterburner Performance
Flight Performance of a Spin-Stabilized 20-Inch-Diameter Solid-Propellant Spherical Rocket Motor
PROPULSION SYSTEM EVALUATION THROUGH FLIGHT SIMULATION
NASA RESEARCH ON RESISTANCE HEATED HYDROGEN JETS
POTENTIALITIES OF THE RADIOISOTOPE ELECTROSTATIC PROPULSION SYSTEM
NASA RESEARCH ON RESISTANCE-HEATED HYDROGEN JETS
THRUST MEASUREMENTS OF COLLOIDAL PARTICLES AS AN INDICATION OF PARTICLE SIZE AND THRUSTOR OPERATION
Performance study of a repetitively pulsed two-stage plasma propulsion engine Final report
Performance Study of a Repetitively Pulsed Two-Stage Plasma Propulsion Engine Final Report
Lunar mission performance evaluation procedure for orbit-launched nuclear vehicles
Aerodynamics and flying qualities of jet v/stol airplanes.
Advanced post-saturn earth launch vehicle study executive summary report
Transient pressure measurements in liquid propellant rocket thrust chambers.