Engine-integrated secondary injection side- force generation for the hydrogen-fueled rocket engine
Engine-integrated secondary injection side-force generation for hydrogen-fueled rocket engine
HYDROGEN FUEL↗
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Results for “ENGINES - HORSEPOWER”
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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High-lift characteristics of a variable-sweep supersonic transport model with a blended engine-fuselage and engine-mounted horizontal tails
High lift characteristics of variable-sweep transport model with blended engine-fuselage and engine-mounted horizontal tails
VARIABLE SWEEP↗
Low-speed characteristics of a variable-sweep supersonic transport model with a blended engine fuselage and engine-mounted tails
Low-speed characteristics of variable-sweep supersonic transport model with blended engine fuselage and engine-mounted tails
FLIGHT CHARACTERISTICS↗
Two surveys of the needs of engineering schools in the field of biomechanical and human factors engineering education
Surveys of engineering school needs in field of biomechanical and human factors engineering education
Glaser, A. A.↗
Computer and engine performance study of a generalized parameter fuel control for jet engines
Computer and engine performance study of jet engine generalized parameter fuel control
Gold, H.↗
Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 1
Thermodynamic performance test analyses for Apollo spacecraft ascent, descent, and service propulsion system engines to define hypergol engine restart limits
Foley, M. G.↗
Engine restart and thermodynamic analysis of Apollo spacecraft engine tests, volume 2
Cold flow and hot firing test details for Apollo spacecraft ascent, descent, and service propulsion system engines to define hypergol engine restart limits
Foley, M. G.↗
Summary of fluid mechanics and engine characteristics research on the nuclear light bulb engine concept
Fluid mechanics and engine dynamics and start-up experiments simulating thermal environment in nuclear light bulb engine
Kendall, J. S.↗
Coupled supersonic inlet-engine control using overboard bypass doors and engine speed to control normal shock position
Coupled supersonic inlet-engine control using overboard bypass doors and engine speed to control normal shock position
Cole, G. L.↗
Validation of the gas generator method of calculating jet-engine thrust and evaluation of XB-70-1 airplane engine performance at ground static conditions
Validating gas generator method of calculating jet engine thrust, and evaluation of XB-70-1 engine performance at ground static conditions
Arnaiz, H. H.↗
Practical engineering methods for predicting hot gas reingestion characteristics of V/STOL aircraft jet lift engines
Engineering methods for predicting temperatures and velocities in vicinity of vertical lift engines of jet V/STOL aircraft operating near ground
Gray, L.↗
Effects of engine inlet disturbances on engine stall performance
Effects of engine inlet disturbances on engine stall performance
Burcham, F. W., Jr.↗
A supersonic inlet-engine control using engine speed as a primary variable for controlling normal shock position
Supersonic inlet engine control using engine speed as primary variable for controlling normal shock position
Hagedorn, R. E.↗
Experimental quiet engine program. Volume 1, phase 1 - Engine design report
Turbofan engine designs and tests for engine noise reduction
Source record↗
Experimental quiet engine program. Volume 2, phase 1 - Engine design report
Low pressure turbofan rotor, stator, frame, and exhaust nozzle designs for turbofan engine noise reduction including acoustics and engine tests
Source record↗
The open-cycle gas-core nuclear rocket engine - Some engineering considerations.
A preliminary design study of a conceptual 6000-MW open-cycle gas-core nuclear rocket engine system was made. The engine has a thrust of 44,200 lb and a specific impulse of 4400 sec. The nuclear fuel is uranium-235 and the propellant is hydrogen. Critical fuel mass was calculated for several reactor configurations. Major components of the reactor (reflector, pressure vessel) and the waste heat rejection system were considered conceptually and were sized.
Taylor, M. F.↗
Multispectral scanner system for ERTS: Four band scanner system. Volume 2: Engineering model panoramic pictures and engineering tests
This document is Volume 2 of three volumes of the Final Report for the four band Multispectral Scanner System (MSS). The results are contained of an analysis of pictures of actual outdoor scenes imaged by the engineering model MSS for spectral response, resolution, noise, and video correction. Also included are the results of engineering tests on the MSS for reflectance and saturation from clouds. Finally, two panoramic pictures of Yosemite National Park are provided.
Source record↗
Summary of engine design and analytical studies to mature the 1137400E engine baseline
Activities in packaging components into integral module arrangements compatible with engine design requirements for the 1137400E flight engine baseline are summarized along with the applied mechanics and thermal analysis. Revisions to drawings, configurations, and support structures are discussed.
Kleinert, D. E.↗