Low-energy proton damage effects in silicon surface-barrier detectors.
Low energy proton damage effects on silicon surface barrier transmission detectors to predict device lifetime in earth radiation belts conditions
Coleman, J. A.↗
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Results for “Love”
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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Normal modes of a nonuniform plasma.
Driven oscillations of electron plasma with sheath described by driven normal mode model
Larson, R. W.↗
Effect of damage by 0.8 Mev - 5.0 Mev protons in silicon surface-barrier detectors.
Proton irradiation damage effects on current and noise in Si surface barrier transmission detectors for nuclear radiation
Coleman, J. A.↗
Earth orbital logistics spacecraft - Performance aspects and vehicle concepts.
Supersonic performance of logistics spacecraft, giving special attention to return from orbit to continental U.S.
Love, E. S.↗
Some topics in hypersonic body shaping.
Hypersonic body shaping for minimum drag and improved performance from view of flight regimes, discussing implications of pressure laws
Ashby, G. C., Jr.↗
Normal mode representation of the high- frequency properties of an inhomogeneous plasma.
Normal mode representation of HF properties of inhomogeneous plasma, analyzing Vlasov equation for free oscillations under external driving field
Leavens, W. M.↗
An experiment on the MHD-driven flow for a gas core nuclear rocket.
Fluid dynamic simulation of gas core nuclear rocket chamber for separating light and heavy gas via centrifugal force produced by MHD-driven rotational flow
Love, W. L.↗
Toward efficient shuttle service to earth orbit.
Low cost efficient shuttle system for personnel and cargo transport to earth orbit for NASA and DOD needs
Love, E. S.↗
Resolution Study
Resolution effects on cartographic data using conventional stereoplotters with photographs taken at orbital heights
Loving, H. B.↗
An experiment on the MHD-driven rotating flow for a gas core nuclear rocket
Gas core nuclear rocket engine light and heavy species centrifugal separation by MHD-driven rotating flow, discussing fluid dynamic simulation results
Love, W. L.↗
Realistic interaction calculations of /p,n/ reactions including tensor knock-out amplitudes
Explore the source record for details and available documents.
Love, W. G.↗
Design of bodies for low drag and high performance in practical hypersonic flight
Minimizing drag and increasing performance of optimum shapes at hypersonic flight
Love, E. S.↗
Evaluation of effects of high-altitude turbulence encounters on the XB-70 airplane
Evaluating effects of high altitude turbulence encounters on XB-70 airplane
Larson, R. R.↗
Gas core nuclear rocket with fuel separation by MHD driven rotation
Operating characteristics and performance predictions for gas-core nuclear rocket with fuel separation by MHD-driven rotation
Love, W. L.↗
Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 1: Mach number 5 booster proximity data
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster proximity data, Mach number 5
Trimmer, L. L.↗
Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 2: Mach number 5 orbiter proximity data
Space Shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter proximity data, Mach number 5
Trimmer, L. L.↗
Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0. Volume 3: Mach number 3 booster proximity data
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - booster proximity data, Mach number 3
Trimmer, L. L.↗
Space shuttle: Investigation of the McDonnell-Douglas orbiter and booster shuttle models in proximity at Mach numbers 2.0 to 6.0 Volume 4: Mach number 3 orbiter proximity data
Space shuttle abort stage separation wind tunnel tests of orbiter and booster vehicles - orbiter proximity data, Mach number 3
Trimmer, L. L.↗