Noise studies of inlet-guide-vane--rotor interaction of a single-stage axial flow compressor
Noise elimination in inlet-guide-vane - rotor interaction of single stage axial flow compressor
COMPRESSOR ROTOR↗
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Results for “Staging”
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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Test-stand study of a vehicle upper stage employing a rotating solid-rocket attitude control system and a comparison with analog studies
Rotating solid rocket control system - test stand study of vehicle upper stage, and comparison with analog studies
ROTATING VEHICLE↗
Technical development status of the s-ic stage - saturn v launch vehicle.
Technical development status of S-IC stage of Saturn V launch vehicle
SATURN V LAUNCH VEHICLE↗
Saturn v s-ic stage engine gimbal actuation system.
Saturn V S-IC stage engine guidance, flight control and gimbal servoactuation system for Apollo spacecraft
SERVOACTUATOR↗
Practical problems in design of high- performance multilayer insulation system for cryogenic stages.
Design problems of high-performance multilayer insulation systems using evacuated flexible-jacket scheme for cryogenic stages
PROPELLANT TANK↗
Development of a lightweight external insulation system for liquid-hydrogen stages of the saturn v vehicle.
Lightweight external insulation system for liquid hydrogen stages of Saturn V vehicle
CRYOGENIC STORAGE↗
Saturn stage S-I-8 final static test report
Static testing of Saturn stage S-1-8 under simulated flight conditions
SATURN LAUNCH VEHICLE↗
Study for improvement of ground test, instrumentation systems, and methods - New methods for stage propellant tank proof testing Final report, 2 Apr. - 1 Dec. 1965
High density, water based slurries for hydrostatic testing of stage propellant tanks
HYDROSTATICS↗
Supersonic investigation of effects of configuration geometry on pressure-coefficient and section normal-force-coefficient distributions for a two-stage launch vehicle
Supersonic study of configuration geometry effects on pressure-coefficient and section normal-force- coefficient distributions for two-stage launch vehicle
SUPERSONIC PRESSURE DISTRIBUTION↗
Development of a proportional two stage pressure feed back pneumatic valve for 2000 deg F solid propellant systems Report, Jul. 6, 1965 - May 20, 1966
Proportional two-stage valve with closed loop pressure feedback logic for high temperature solid propellant pneumatic system
CLOSED LOOP SYSTEM↗
A day-night high resolution infrared radiometer employing two-stage radiant cooling, volume I First quarterly report, 1 Jan. - 1 Apr. 1966
Two-stage radiant cooler for infrared detector in day-night high resolution radiometer on Nimbus- type spacecraft
RADIATION COOLING↗
Improvements in stage checkout
Test methods, equipment, and computer programs for improved quality control in space vehicle stage checkout
CHECKOUT EQUIPMENT↗
Investigation of a lightweight self-evacuating prefabricated multi-layer insulation system for cryogenic space propulsion stages Final report, 3 Jun. 1965 - 31 Jul. 1966
Lightweight self-evacuating prefabricated multilayer insulation system for cryogenic space propulsion stages
MULTILAYER STRUCTURE↗
Performance evaluation of three-stage prototype NERVA turbine designed for blade-jet speed ratio of 0.107
Performance evaluation of three-stage prototype NERVA turbine designed for blade-jet speed ratio of 0.107
PERFORMANCE CHARACTERISTICS↗
Three-stage hardening in tantalum single crystals.
Three-stage hardening in tantalum single crystals deformed in tension over limited range of orientations, temperatures and strain rates
BODY CENTERED CUBIC /BCC/ CRYSTAL↗
Definitive determination of the ionization stage for spectral lines.
Ionization charge stage for spectral lines determined by sending particle beam through field which separates components of different net charge
VAN DE GRAAFF ACCELERATOR↗
Steady state operation of a two-stage pulsed coaxial plasma engine.
Performance characteristics of two-stage pulsed coaxial plasma engine
ELECTRIC PROPULSION↗