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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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Conversion by electrochemical process of chemical to electrical energy - high energy compounds in organic electrolytes and cathode materials
Properties of ferroelectric and ferromagnetic compounds of manganite with rare earths
Silicone rubber adhesives and potting compounds - polymeric materials for spacecraft
Effect of environmental temperatures and relative humidities on curing times of polyurethane and polysulfide potting compounds
High energy compounds in organic electrolytes - electrochemical and chemical properties of cyclic esters, gamma butyrolactone, gamma valerolactone, and propylene carbonate
Thermodynamic properties of various carbon- hydrogen-nitrogen-oxygen-phosphorus-sulfur compounds
Bibliography on electrochemistry of high energy compounds in organic electrolytes
Nuclear magnetic resonance of phosphorus compounds, discussing signs of spin-spin couplings in dimethylphosphine and methylphosphine
Mass spectrometry and gas chromatography in analysis of organic compounds present in extraterrestrial bodies to provide information on existence of life
Crystal structure of some ternary intermetallic titanium compounds
Sterilizable potting compounds and conformal coatings for space applications
Electrochemistry of high energy compounds in organic electrolytes
Screening of inorganic compounds as solvents for electrolytes in high energy density battery systems
Complex organic compounds analysis by fast- electrical-scanning high resolution mass spectrometry and gas chromatography
Aromatic compounds in benzene eluate fractions from carbonaceous chondrites by high resolution capillary gas-liquid chromatography
Identification of nitrogenous compounds in orgueil meteorite
Presents an analysis of a compound engine operating with manifold pressures ranging from 60 to 110 lb/sq in. absolute. The effects of engine limits (peak cylinder pressure and turbine-inlet temperature) and component efficiency are discussed. A range analysis is used to evaluate the merit of the engine. The analysis indicates that specific-fuel-consumption values of 0.32 lb/bhp-hr and specific weights of 0.8 lb/bhp are obtainable at high manifold pressures.
The potential of the semiconducting compound Beta-Zn(sub 4)Sb(sub 3) for thermoelectric energy conversion was investigated. The thermoelectric properties were measured on hot-pressed samples characterized by x-ray and microprobe analysis.