Apollo RCS Positive Expulsion Tankage Product Improvement Program. Task B - Long Term Compatibility Testing Final Report, Jul. 1967 - Sep. 1969
Useful operating life of Apollo and LM RCS propellant tank configurations
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Useful operating life of Apollo and LM RCS propellant tank configurations
Weightless containerless processing for space, electromagnetic position control, force measurements and techniques, and hydrodynamics
Design optimization of lateral p-n-p transistors with minimum processing steps
Outgassing apparatus and gas analysis data for modular nuclear vehicle
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - vacuum seal valves
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - low heat cryogenic rotary joint
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - vacuum probes
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - central vacuum pulldown system
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - bayonet joints in cryogenic propellant and vent lines
Dynamic model for effects of random scanning and sampling on human operator tracking performance
Melting and handling of molten material in weightless space environment
Facility modification plan for testing 260-inch diameter solid rocket engine
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