Tracking System Data Analysis Report, Ranger 4 Final Report
Deep space instrumentation facility /dsif/ spacecraft tracking performance during ranger iv lunar probe mission
DEEP SPACE INSTRUMENTATION FACILITY /DSIF/↗
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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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A computer solution for hydrostatic bearings with variable film thickness final technical report
Computer solution for hydrostatic bearings with variable film thickness
COMPUTER METHOD↗
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
PYROLYTIC GRAPHITE↗
Development of improved thermoelectric materials for spacecraft applications final summary report, apr. 29 - jul. 29, 1964
Thermoelectric and thermomagnetic cooling and material development for spacecraft application
THERMOELECTRIC MATERIAL↗
A transducer for the continuous external measurement of arterial blood pressure final report
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Newgard, P. M.↗
Evaluation of liquid sterilants, phases iii, iv, v, vi, and vii final report
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English, E. G.↗
Microlock beacon evaluation study final report
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Kelly, F. G.↗
One frame delta encoder final report
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Hackett, K. R.↗
An analytical study of digital control systems for flight vehicles final report
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Source record↗
Final preliminary design and technical report for study of advanced antenna system for the deep space instrumentation facility volume i
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Investigation of thermionic energy conversion final report, 9 jul. - 9 sep. 1962
Refractory ceramic oxide for thermionic diodes
CERAMICS↗
Liquid propellant losses during space flight final report, sep. 1, 1960 - sep. 30, 1963
Multilayer insulation for liquid hydrogen propellant tanks in space environment
SPACE ENVIRONMENT↗
Design aspects of explosive mixtures in a vehcile interstage final report
Prevention and control of explosive mixture of hydrogen and oxygen within vehicle interstage
EXPLOSIVE↗
Aerodynamic characteristics from mach 0.22 to 4.65 of a two-stage rocket vehicle having an unusual nose shape high power, high voltage, audio frequency transformer design manual final report, 1 jul. 1962 - 31 aug. 1964
Transonic and supersonic aerodynamic characteristics for two-stage rocket vehicle with blunted nose cone on square body with conical flare termination
ROCKET VEHICLE↗
Mechanics of deformations and fracture final report
Thermal analysis of mechanical behavior of material models with temperature dependent properties
MECHANICAL PROPERTY↗
106 bit engineering recorder/reproducer final engineering report no. 607
Magnetic tape recorder-reproducer for Mariner planetary space vehicles
MAGNETIC TAPE RECORDER↗
Thermal energy storage research and development program final technical report, 6 dec. 1960 - 1 dec. 1961
Thermal energy storage materials for use in solar thermionic power spacecraft systems
THERMIONIC CONVERSION SYSTEM↗
Design study of a high power in-pile nuclear thermionic space powerplant final report
Thermionic nuclear spacecraft power plant
SPACECRAFT POWER SUPPLY↗