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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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RESEARCH STUDY TO DETERMINE PROPULSION REQUIREMENTS AND SYSTEMS FOR SPACE MISSIONS VOL. 1 FINAL REPORT, <COVERING PERIOD< FEB. 1, THRU OCT. 31, 1961
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RESEARCH STUDY TO DETERMINE PROPULSION REQUIREMENTS AND SYSTEMS FOR SPACE MISSIONS VOL. II A FINAL REPORT, <COVERING PERIOD< FEB. 1 THRU OCT. 31, 1961
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RESEARCH STUDY TO DETERMINE PROPULSION REQUIREMENTS AND SYSTEMS FOR SPACE MISSIONS VOL. IIB FINAL REPORT, <COVERING PERIOD< FEB. 1 THRU OCT. 31, 1961
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RESEARCH STUDY TO DETERMINE PROPULSION REQUIREMENTS AND SYSTEMS FOR SPACE MISSIONS VOL. III FINAL REPORT, <COVERING PERIOD< FEB. 1 THRU OCT. 31, 1961
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Adhesion between atomically clean metallic surfaces final report
Adhesion between atomically clean metallic surfaces - surface energy and bonding
Propulsion requirements for soft landing in extraterrestrial environments. vol 1-summary and propulsion design guide final report
Summary and propulsion design guide for soft landing in extraterrestrial environments
Pilot theoretical study of the effect of weightlessness and densely ionizing radiation on single cells final report
Effect of weightlessness on single cells
Reduction and analysis of explorer vi and pioneer v data, volume i final report
Explorer vi and pioneer v data reduction and analysis
Tiros 1 Meteorological Satellite System Final Report
Tiros i meteorological satellite system - design, development, operation, engineering evaluation, and meteorological uses of television data
The electronic transition moment for the schumann-runge band system of oxygen research directed toward theoretical and experimental investigation in laboratory astrophysics involving shock heated high temperature gases final report
Electronic transition moment for schumann-runge band system of oxygen - nuclear physics
Cloud pattern interpretation <final report<
Recognition of cloud pattern from films taken by tiros satellite
Spacecraft engine thrust chamber cooling final report, 13 may 1963 - 12 apr. 1964
Cooling thrust chamber of liquid propellant rocket engine using pyrolytic graphite and hydrocarbon film
A transducer for the continuous external measurement of arterial blood pressure final report
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Evaluation of liquid sterilants, phases iii, iv, v, vi, and vii final report
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Microlock beacon evaluation study final report
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One frame delta encoder final report
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An analytical study of digital control systems for flight vehicles final report
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