SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Rotor design to evaluate outer case blowing or bleeding of single stage axial flow compressor
Construction and testing of two-stage radiant cooler for day and night high resolution infrared radiometer
Simulated bearing coolant injection effect on performance of two stage, velocity compounded turbojet drive turbine
Piloted simulation of manual guidance techniques for upper stages of Saturn V launch vehicle
Downstream stator contribution to interaction noise of single-stage axial flow compressor
Analyses of aspect ratio and curvature variations for axial flow compressor inlet stages under loading
Space vehicle stage checkout in Saturn launch application
Partial admission performance characteristics of single stage supersonic turbine
Two magnetically geared microscope stages for nuclear track plates
Oxidation of Al-2 percent aluminum oxide SAP TYPE alloy foil heated in situ and observed by hot stage transmission microscopy, electron diffraction and motion picture micrography
High energy booster and upper stage combinations for space research, discussing mission capabilities, cost factors, reliability, etc
Reliability methodology in design and development stage, discussing component stresses, performance variation, etc
Computer applications in checkout of individual Saturn stages and in prelaunch checkout of complete Saturn vehicle
Performance and feasibility of staged propulsion during terminal phase of Mars soft landing
Spacecraft configurations and propulsion system module design for Voyager project, based on lunar module descent stage applications
Modified computer program using finite difference method for calculating base flow field and dissipation for Saturn S-2 stage
Final flight performance prediction for Saturn AS-204 LM propulsion system S 1B stage
Feasibility study and capability evaluation of 44-inch first stage rocket motor for Scout vehicle