An instrumentation system to study rocket exhaust plume radiative processes Final report
Instrumentation system for studying radiative heat transfer from exhaust plume of liquid oxygen- RP-1 rocket fuel
RADIATIVE HEAT TRANSFER↗
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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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Observation of the GT-5 rocket-body reentry - Preliminary analysis
Observation of GT-5 rocket body reentry - preliminary analysis of second stage of Titan launch vehicle
SECOND STAGE↗
Static aerodynamic characteristics of a rocket vehicle with thick wedge fins and sweptback leading and trailing edges
Static aerodynamic characteristics of rocket model vehicles with thick wedge fins with sweptback leading and trailing edges - supersonic wind tunnel testing of vehicle longitudinal stability
ROCKET VEHICLE↗
Ion rocket system research and development Final report, 24 Feb. 1964 - 25 Jun. 1965
Design studies and testing of ion rocket engine and zero gravity feed system
ROCKET ENGINE↗
Analytical study of hydrogen turbopump cycles for advanced nuclear rockets Progress report, Sep. 15, 1964 - Sep. 15, 1965
Hydrogen turbopump cycles for obtaining high engine inlet pressures in advanced nuclear rockets, and data on gaseous nuclear reactors and heavy gas containment
HYDROGEN↗
A study to define a state-of-the-art rocket vehicle suitable for synoptic meteorological soundings, volume 1 Final report
Rocket vehicle for synoptic meteorological soundings - evaluation of four proposed systems
SOUNDING ROCKET↗
Steady state aerothermochemistry for liquid bipropellant rocket motors
Model and theoretical equations describing liquid propellant droplet ballistics and combustion gas behavior in bipropellant rocket motors - aerothermochemistry
LIQUID PROPELLANT ROCKET ENGINE↗
Vortex flow and erosion in rocket nozzles due to warm-gas injection for thrust vector control
Vortex flow and erosion in rocket nozzles from warm-gas injection for thrust vector control
THRUST VECTOR CONTROL /TVC/↗
Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. I - Inlet feedpipe-manifold assembly
Cold air performance of scale model oxidizer pump drive turbine feedpipe-manifold-nozzle assembly for M-1 rocket engine
COLD FLOW TEST↗
Nuclear rockets based on graphite reactor technology - Their applications and development status
Development and mission applications of nuclear rockets based on graphite reactor technology
MISSION PLANNING↗
High resolution radio frequency measurements of Faraday rotation and differential absorption with rocket probes
System and operating techniques for high resolution radio frequency measurements of Faraday rotation and differential absorption in lower ionosphere using rocket probes
RADIO FREQUENCY↗
Evaluation of the MARC 7G1 auxiliary rocket motor for use on the Atlas-Centaur vehicle Final report, Mar. - Oct. 1965
Solid propellant rocket engine environmental and static testing for use as retrograde thrustor in Atlas-Centaur space vehicle
ATLAS CENTAUR LAUNCH VEHICLE↗
Gas mixtures for dynamic simulation of rocket exhaust jets Final progress report, 12 Apr. - 11 Nov. 1965
Screening and evaluation of gas mixture for dynamic simulation of rocket exhaust jets
GAS MIXTURE↗
Catalysis of hydrogen-atom recombination in rocket nozzles
Oxygen and oxygen-nitrogen mixtures as catalysts for hydrogen atom recombination in rocket nozzles
CATALYST↗
Experimental evaluation of various nonmetallic ablative materials as nozzle sections of hydrogen-oxygen rocket engine
Evaluation and erosion of nonmetallic ablating materials as rocket nozzle sections
ROCKET NOZZLE↗
Rocket measurements of Sq currents at mid-latitude
Double gas cell rubidium vapor magnetometers in Nike-Apache rockets and ionospheric current detection
NIKE-APACHE ROCKET↗
Rocket Measurements of the Geomagnetic Field Above Woomera, South Australia
Geomagnetic field measurements from rockets using proton magnetometer
GEOMAGNETIC FIELD↗
Ion rocket engine development Quarterly report no. 3, 1 Apr. - 30 Jun. 1965
Integral focus cesium contact ion rocket engine and iridium and rhenium coated porous tungsten ionizer evaluations
IRIDIUM↗