Analysis of the longitudinal high frequency stability of a staged combustion cycle, Appendix B
Time lag theory for longitudinal high frequency stability analysis on staged combustion cycle of liquid propellant rocket engine
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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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Single stage experimental evaluation of compressor blading with slots and wall flow fences
Additional slot and flow fence effects on aerodynamic characteristics of single stage compressor blading
Brent, J. A.↗
Computer program describing turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for a two stage axial flow turbine
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for two stage axial flow turbine
Evans, D. G.↗
Lateral displacement system for separated rocket stages Patent
Development of remotely controlled shaped charge for lateral displacement of rocket stages after separation
Blanchard, W. S., Jr.↗
Hard X-ray evidence for two stage particle acceleration in a solar flare
Hard X-ray evidence for two stage particle acceleration in solar flare
Dennis, B. R.↗
Prospects for a multipurpose solar electric propulsion stage
Technology review and performance estimates for fixed design multipurpose solar electric propulsion stage
Hrach, F. J.↗
Cold air investigation of a turbine with transpiration cooled stator blades 4 - Stage performance with wire-mesh shell stator blading
Cold-air tests to determine performance characteristics of single-stage turbine with stator blades employing transpiration coolant ejection through wire mesh shell
Behning, F. P.↗
Exponential downweighting of past data in a single stage, weighted-least-squares trajectory processor
Exponential downweighting of past data in single stage, weighted least squares trajectory processor for coasting spacecraft
Rich, R. G.↗
Plume impingement during separation of a two stage space shuttle vehicle
Optimum separation trajectory analysis for two stage space shuttle configuration considering plume impingement effect
Fossler, I.↗
Three stage potassium vapor turbine test
Three-stage potassium vapor turbine test to determine effects of vapor wetness on impingement damage of different rotor blade materials
Moor, B. L.↗
Performance of a ten-stage electrostatic depressed collector for klystrons
Computational method for determining performance of ten stage electrostatic depressed collector for klystrons
Mihran, T. G.↗
Study of a common solar-electric-propulsion upper stage for high-energy unmanned missions. Volume 1 - Summary Final report
Versatile, multimission solar electric propulsion upper stage for high energy, unmanned interplanetary flights - summary
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Study of a common solar-electric-propulsion upper stage for high-energy unmanned missions. Volume 2 - Technical Final report
Versatile, multimission solar electric propulsion upper stage for high energy, unmanned interplanetary flights - technical details
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Study of a common solar-electric-propulsion upper stage for high-energy unmanned missions. Volume 3 - Appendixes Final report
Versatile, multimission solar electric propulsion upper stage for high energy, unmanned interplanetary flights - appendices
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Scout first stage flight characteristics
Scout first stage jet vane effectiveness, and aerodynamic pitching and yawing moment coefficients determined from flight data
Knauber, R. N.↗
Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 2 Final report
Computer output tables for performance tests of single stage, transonic compressor for advanced aircraft
Bilwakesh, K. R.↗
Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1 Final report
Performance tests of single stage, transonic compressor for advanced aircraft
Bilwakesh, K. R.↗
Design, fabrication, and static testing of first-stage Attached Inflatable Decelerator (AID) models
Design, fabrication, and static testing of wind tunnel models of first-stage Attached Inflatable Decelerator canopies for supersonic vehicles
Johnson, B. A.↗