Thermionic spacecraft design study Phase 1 report, 4 Feb. 1969 - 4 Jan. 1970
Design of nuclear electric propelled unmanned spacecraft
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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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Design of nuclear electric propelled unmanned spacecraft
Charge transfer processes in synthesis of polymers
Low energy neutral detection, bremsstrahlung spectra emitted from dense plasma focus mode of plasma accelerator, atomic processes and solid state physics
Uniform adhesive shear stress distributions in double-lap bonded joints and joint design criteria
Statistical analysis of neural pulse frequency modulator
Design and testing of intravehicular activity space suit
Design to improve emittance performance of louver system for thermal control of Pioneer 4
Nondestructive test methods for Saturn program Zener diodes evaluated to develop screening procedures for potential failures
Evaluating toxicity of propellant within space station, leakage criteria of propellant and nitrogen, and weight comparisons of five candidate resupply systems - graphs
Literature survey of redundant systems for spacecraft data systems reliability analysis
Data acquisition instrumentation for heartbeat display in electrocardiogram
Quality control failure analysis on silicon microcircuit structures
Prototype test model of 30-watt per pound rollup solar array
Mathematical model for performance prediction of silicon solar cell in space environment
Advanced electrocatalyst performance and electrode fabrication for fuel cells
Field ion microscopy of stoichiometric platinum and nickel alloys for atomic ordering parameters
Summary of radio observatory activities concentrating on polarization and short time resolution burst structure of radiation
Tunable optical sources by means of nonlinear optical techniques