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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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Jet pluming effect on static stability of five cone cylinder-flare finned rocket models at Mach numbers of 4, 5, and 6 and static pressure ratios up to 26,000
Rocket and satellite measurements on meteoritic dust
Heat and mass transfer characteristics of axial- flow liquid-core nuclear rocket engine employing radiation heat transfer
Numerical method for rocket trajectory determination from multistation Doppler tracking data
Recovery of reentry rocket by sound ranging detection of shock wave
Axial mode shock wave combustion instability in liquid propellant rocket engines
Compendium of Aerobee sounding rocket launchings for 1964
Nonlinear aspects of combustion instability in liquid propellant rocket engines
Chamber pressure variations and rocket combustor performance for gaseous hydrogen-liquid oxygen propellant system
Test firing evaluation of six ablative-material thrust chambers as components of storable propellant rocket engines
Integrated rocket spin-up launch mechanism with pyrotechnic and mechanical events initiated by single electric signal
Inhomogeneous radiant heat transfer from Saturn rocket exhaust plumes
Hydrodynamic differential and difference equations and computer algorithm for nonlinear combustion instability in liquid propellant rocket engines, and Fortran IV listing
Multiple start-stop solid propellant rocket motor using highly aluminized ammonium perchlorate annular propellant grains
Far ultraviolet polarization analyzer for rocket measurement of resonantly scattered sunlight
Equatorial ionospheric propagation studies using rocket sounding techniques
Rocket explosion air blast parameters and design in relation to structural load calculations
Revised computer program on feasibility of water injection-cooled diffuser for nuclear rocket engine/stage test stands