The Significance of the Time Concept in Engine Detonation
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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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This presentation is a program update for the members of the JANNAF RDRE Panel. There is no technical content. A list of NASA sponsored projects is provided, along with the motivation for NASA’s involvement in the development of this type of propulsion system, and key technology gaps that need to be addressed.
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Poster summarizing STMD Game Changing Development RDRE Project
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Shock wave ignition of hydrogen-oxygen-diluent mixtures
Measurement of fission products from Star Fish high-altitude nuclear explosion with recording gamma-ray spectrometer
Measurements of rotating pressure wave about combustion chamber axis during resonant combustion of liquid propellant rocket engine
Combustion instability in liquid propellant rocket motors causing pressure fluctuations
Shock tube simulation of rocket exhaust plumes and effects on vehicles in space environment
Shock tube simulation of rocket exhaust plumes and effects on vehicles in space environment
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Sensitivities of various metal/halocarbon slurries to impact are given. Barium and lithium shavings show sensitivity with all of the halocarbons tested except methyl chloroform. Powdered aluminum, magnesium titanium, and beryllium show sensitivity with several halocarbons but generally require a higher level of initial energy.
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Shape and inner flow of a tridimensional spark are studied. The spark is created by focusing a laser beam in a gas. A second order fully non-linear equation is derived for the radial velocity on the axis of symmetry in the neighborhood of the origin. Solutions to that equation display the existence of a forbidden region near the focus, thus indicating the limits of applicability of a small perturbation solution.
Simulation of rocket plumes and reentry aerothermodynamics using oxygen/hydrogen combustion products