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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Cavecche, E. H.↗
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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. IVA
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Cavecche, E. H.↗
ASTRONAUTICS INFORMATION. OPEN LITERATURE SURVEY, VOL. II, NO. 6
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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
SOFT LANDING↗
Satellite situation report, vol. 4, no. 6
Table of objects in orbit - name, source, launch, period, inclination, apogee, perigee, and frequency
ORBITAL ELEMENT↗
The state of carbon in titanium, tantalum, and tungsten <pro stan vugletsyu v titani, tantali ta vol'frami<
Carbon ion mobility change in titanium, tantalum, & tungsten
ION MOBILITY↗
Space operations control center satellite situation report, vol. 5, no. 3
Orbiting satellite situation report
SATELLITE ORBIT↗
Space operations control center satellite situation report, vol. 5, no. 5
Catalog of orbiting space satellites, debris, and satellite lifetimes
ORBITING SATELLITE↗
Satellite situation report, vol. 5, no. 4
Orbital elements for satellite objects in orbit, launching list for years 1958 through 1965, and decayed objects list
ORBITING SATELLITE↗
Saturn i, launch vehicle sa-10 and launch complex 37b functional systems description. vol. vi- environmental conditioning systems, functional description, index of finding numbers, and mechanical schematics
Saturn I /SA-10/ launch vehicle and Launch Complex 37B functional systems description - environmental conditioning, index of finding numbers, and mechanical schematics
SATURN I /SA-10/ LAUNCH VEHICLE↗
Performance evaluation of 'thermo-lag' material for entry heat protection of advanced manned spacecraft. vol. 1- summary of investigations final report, 1 oct. 1962 - 31 jan. 1964
Thermoconductivity and thermal properties of protective coating and structural material for reentry manned spacecraft
STRUCTURAL MATERIAL↗
Performance evaluation of ''thermo-lag'' material for entry heat protection of advanced manned spacecraft. vol. 2- thermal investigations final report, 1 oct. 1962 - 31 jan. 1964
Thermal properties and performance of Thermo-lag material for entry heat protection of manned spacecraft
MANNED SPACECRAFT↗
Performance evaluation of ''thermo-lag'' material for entry heat protection of advanced manned spacecraft. vol. 3- structural investigations final report, 1 oct. 1962 - 31 jan. 1964
Mechanical properties and structural analysis of Thermo-lag material for entry heat protection of manned spacecraft
MANNED SPACECRAFT↗
Performance evaluation of ''thermo-lag'' material for entry heat protection of advanced manned spacecraft. vol. 4- blister investigations final report, 1 oct. 1962 - 31 jan. 1964
Chemical analysis of blistered cones for performance evaluation of Thermo-lag material for entry heat protection of manned spacecraft
MANNED SPACECRAFT↗
A technique for precise analysis of satellite data. vol. ii- radiation analysis. section 6- fixed-position scanning
Fixed position scanning by TIROS satellite for photogrammetric analysis of cloud photographs
CLOUD PHOTOGRAPH↗
Juncture stress fields in multicellular shell structures. Vol. IX - Summary of results and recommendations Final report
Juncture stress fields in multicellular shell structures - bending and bucking analyses
BUCKLING↗
A transient heat transfer and thermodynamic analysis of the Apollo service module propulsion system. Vol. I, phase I - Transient thermal analysis Final report, 28 Jul. 1964 - 28 Jul. 1965
Transient heat transfer and thermodynamic behavior analysis for Apollo service module propulsion system - fuel cell effect on overheating
THERMODYNAMIC PROPERTY↗