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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Simulation of cargo transfer in weightlessness environment
German analysis of preparatory technology of U.S. space programs, noting effects of hardware development for manned space travel on future planning
Simultaneous electrocardiographic and phonocardiographic data obtained from Gemini flights
Chronology on aerospace events and personalities
Predicting star magnitude visible through contaminated spacecraft window by naked eye or sextant
Mercury, Gemini, and Apollo manned flight operational and personnel data
Prototype lunar gravity simulator for studies of reduced gravity effects on human self locomotive capability, using magnetic air bearings and body support system
Dosimetry data and personal radiation sensors from Apollo and Gemini flights, noting spacecraft geometry shielding effects
Aerospace thermophysics considerations in spacecraft and hypervelocity vehicles systems thermal design, discussing thermal control and control coatings optical and radiative properties
Monitoring techniques for biological and chemical atmospheric contaminants in closed environment
Statistical mechanics for wall shear turbulence in Couette flow based on Brownian motion and comparison with stochastic theory based on Navier-Stokes equation
Measuring instruments for in vivo bone mineral content and body composition measurement
Human exposure to particulate radiation and energetic X rays
Unmanned lunar logistics vehicle for extended manned lunar exploration support, discussing general design, propulsion and control systems
Apollo hybrid simulator for man-machine interface in low orbit lunar landmark tracking
Two problem areas are reviewed: (1) the nature of and approach to the EVA mission and (2) the guidance and stabilization required of such a mission. The report indicates several broad areas in which additional research is needed to provide an advance to the state-of-the-art. Moreover, the research problems cited were chosen from among many as those most amenable to research and study in the university environment.
A brief description is given of the schemes suggested for providing electrical power aboard spacecraft. An attempt was made to list the major advantages and disadvantages of each scheme and to identify the particular areas in which it appears likely further research work may prove fruitful. Special attention was given to those research areas that appear suitable for colleges and university work. Chemical, solar, and nuclear power sources are considered together with the appropriate thermoelectric and turboelectric conversion systems.
A comparative study was performed to define an optimum portable life support system for suited operations inside and outside the Skylab Program. Emphasis was placed on utilization of qualified equipment, modified versions of qualified equipment, and new systems made up to state-of-the-art components. Outlined are the mission constraints, operational modes, and evaluation ground rules by which the Skylab portable life support system was selected and the resulting design.