Determination of processing and test facility requirements for large solid rocket motors. Volume 2 - Task 2 - facility optimization Final report
Cost optimization for 260-inch diameter solid rocket engine test facility
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Cost optimization for 260-inch diameter solid rocket engine test facility
Design and fabrication of full size landing impact test model of Mars legged lander configuration
Design of bladder expulsion device subjected to constraints such as cycle life, chemical inertness, and storability
Thermal control system for space storable propellant module
State space models of remote manipulation problem applied to human supervised or autonomous computer manipulators
Fluid motion in cylindrical tank with arbitrary sector annular cross section subjected to harmonic longitudinal excitation
Thermal control concepts for space storable fluorine hydrazine propulsion module
Spacecraft crew function classification and methods for communicating with onboard computers
Analysis of ranging system for lunar surface electrical properties experiment
Recommendations for future US space program
Results of simulated runs to evaluate lunar module descent performance of P66 automatic control and guidance system
Wettability of microfog streams of high temperature lubricants on static metal surface
Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol. 1
Evaluation of range and distortion tolerance for high Mach number transonic fan stages - Vol. 2
Inlet flow distortion testing of high Mach number transonic fan stages - Vol. 1
Tabular data derived from inlet flow distortion tests of high Mach number transonic fan stages - Vol. 2
Seal ring carbon-graphite materials for aircraft gas turbines
Man machine systems and astronaut and onboard computer communications