Feasibility study for a 44-inch first stage rocket motor Final report
Feasibility study and capability evaluation of 44-inch first stage rocket motor for Scout vehicle
Source record↗
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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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Performance evaluation of a two stage axial-flow turbine for two values of tip clearance
Performance of two-stage axial flow turbine operating at different rotor tip clearance
Kofskey, M. G.↗
Performance in air of 4 inch /10.16-cm/ mean-diameter single stage axial-flow turbine for Reynolds numbers from 4,900 to 188,000
Reynolds number effect on single stage axial flow turbine in air
Klassen, H. A.↗
Two-stage potassium test turbine. Volume 4 - Materials support of performance and endurance tests
Two stage potassium vapor turbine - materials support of performance and endurance tests
Engleby, D. S.↗
Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. 3 - Performance of first stage with inlet-feedpipe-manifold assembly
Cold air performance test of scale model oxidizer pump drive turbine for M-1 engine - performance of first stage with inlet feedpipe manifold assembly
Kline, J. F.↗
Two-stage potassium test turbine. Volume 1 - Fluid dynamic design and performance
Two stage turbine suitable for use in wet potassium vapor at temperatures of 1400 to 1600 deg F
Rossbach, R. J.↗
Aerodynamic evaluation of two-stage axial flow turbine designed for Brayton-cycle space power system
Experimental design and performance test of two-stage axial-flow turbine designed for Brayton-cycle space power system
Kofskey, M. G.↗
Two-stage potassium test turbine. Volume 2 - Mechanical design and development
Mechanical design and development test program for two-stage potassium vapor Rankine cycle turbine
Fink, R. W.↗
A Day-night High Resolution Infrared Radiometer Employing Two-stage Radiant Cooling Quarterly Report, 1 Jul. - 1 Oct. 1967
Thermal testing of two stage radiant cooler for day-night high resolution infrared radiometer
Source record↗
Two-stage potassium test turbine. Volume 3 - Test facilities
Design, and performance of facility for Rankine cycle testing of two stage potassium vapor turbine
Eckard, S. E.↗
Operations and maintenance manual uprated Saturn 1 and Saturn 5 vehicle stage pressurized lighting system
Operations and maintenance manual of uprated Saturn 1 and Saturn 5 vehicle stage pressurized lighting system
Source record↗
Proposed analytical model for the final stages of landing a transport airplane
Simple model describing final airborne stages of landing transport aircraft manually
White, M. D.↗
Two-stage bipropellant injection system studies Final report
Two stage bipropellant injection with high thrust per injector
Mehegan, P. F.↗
A day-night high resolution infrared radiometer employing two-stage radiant cooling. Part 2. Breadboard day-night radiometer Final report
Integrating two-stage radiant cooler into breadboard model of day-night radiometer
Annable, R. V.↗
Final flight performance prediction for Saturn AS-205 propulsion system S-1B-5 stage
Flight performance prediction for Saturn AS-205 propulsion system S-1B-5 stage
Cordes, R. M.↗
Thrust-vector control requirements for large launch vehicles with solid-propellant first stages
Thrust vector control for large launch vehicles with solid propellant first stages
Borsody, J.↗
Single stage experimental evaluation of variable geometry guide vanes and stators. Part 1 - Analysis and design
Variable geometry concepts applied to guide vanes and stators in single stage compressors
Jones, B. A.↗
A device for measuring the spatial orientation between two separating stages of a space vehicle
Design, development, and testing of device for measuring spatial orientation between separating S-2 and S-4B stages of Saturn 5
Source record↗