Test of improved ignitor for first stage separation rockets for the Atlas-Centaur launch vehicle
Development and test firing of improved igniter for first stage retrorockets of Atlas Centaur launch vehicle
Heath, R. W.↗
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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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Power train for three-stage potassium test turbine. Volume 1 - Final design
Final design for power train for three stage potassium test turbine
Fink, R. W.↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 3 - Performance of blowing insert configuration no. 1
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor, and performance tests using distorted or undistorted inlet flow
Koch, C. C.↗
Analytical investigation of the effect of cooling air on two-stage turbine performance
Flow analysis to determine turbine efficiency as function of inlet temperature for two stage turbine
Whitney, W. J.↗
Single stage experimental evaluation of variable geometry guide vanes and stator blading. Part 5 - Overall performance for variable camber guide vane and stator B with radial and circumferential inlet flow distortion
Inlet flow distortion effects on single stage variable geometry guide vanes and stators
Clark, C. E.↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 4 - Performance of bleed insert configuration no. 3
Evaluation of bleed insert configuration of single stage axial flow compressor
Koch, C. C.↗
Effect of rotor tip clearance on the performance of a 5-inch single stage axial flow turbine
Effect of rotor tip clearance on performance of 5-inch single-stage axial flow turbine
Futral, S. M., Jr.↗
Conceptual study of rocket-scramjet hybrid engines in a lifting reusable second stage
Rocket-scramjet hybrid engines in lifting reusable second stage
Allen, J. L.↗
Scout standard 5th stage BE-3-A9 rocket motor propulsion unit program Final report
Modified BE-3 engine for fifth stage of Scout launch vehicle
Robertson, D. R.↗
Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 5 - Performance of plain casing insert configuration with distorted inlet flow
Outer case bleeding or blowing effects on casing insert of single stage axial flow compressor with distorted inlet flow
Koch, C. C.↗
Three-stage potassium vapor turbine fabrication and assembly Final report
Pretest assembly, fabrication and specification records of three stage potassium test turbine hardware
Fink, R. W.↗
Aerodynamic Interference Effects Caused by Parallel-Staged Simple Aerodynamic Configurations at Mach Numbers of 3 and 6
Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach numbers of 3 and 6
Decker, John P.↗
Aerodynamic characteristics in pitch of a 1/7-scale model of a two- and three-stage rocket configuration at Mach numbers of 0.4 to 4.63
Aerodynamic characteristics in pitch of scale model of two and three stage rocket configuration at Mach numbers of 0.4 to 4.63
Fournier, R. H.↗
The development of a space oriented portable work-photographic light in support of S-4B spent stage experiments Final report, 1 Oct. 1968
Portable work-photographic light with miniature circuitry for S-4B spent stage experiments
Source record↗
Development of nondestructive test device for evaluation of 3/4-inch thick polyurethane Spray-On Foam Insulation /SOFI/ on the Saturn S-2 stage
Nondestructive test device for evaluation of polyurethane foam sprayed insulation on Saturn S-2 stage
Haralson, H. S.↗
Propellant selection for unmanned spacecraft propulsion systems. Volume 3 - Study of propulsion stage commonality and attitude control systems requirements, phase 2 Final report
Feasibility of common stage for alternate space missions and attitude control systems for unmanned spacecraft propulsion system
Source record↗
A method for obtaining performance boundaries of complete space propulsion systems containing nuclear-electric stages.
Performance boundaries of space propulsion systems containing nuclear electric stages
Casal, F. G.↗
Saturn V/S-IC stage model and flight test base thermal environment.
Thermal and pressure environments analysis in Saturn S-1C stage base during flight tests, noting base gas flowfield and heating
Bender, R. L.↗