High-performance Thermionic Converters Final Report, 19 May 1965 - 19 Jul. 1966
Precision variable parameter test vehicles for parametric studies of plane-parallel cesium vapor thermionic converter performance
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Precision variable parameter test vehicles for parametric studies of plane-parallel cesium vapor thermionic converter performance
Two-stage, axial flow turbine test rig for providing cold flow aerodynamic performance data on Brayton cycle alternator drive turbine
Compressor research package to provide aerodynamic performance data for Brayton-cycle axial flow turbomachinery
Thermal design of aluminized Mylar insulation system for cryogenic storage tanks - helium purging
Diffusion coefficients, outgassing studies, and correlation of complete system thermal model computer program predictions with 82.6 inch tank test data
Design and performance testing of large scale mixed compression axisymmetric inlet at transonic and supersonic speeds
Engineering analysis for evaluating moving bed and mediator hydrogen-oxygen fuel cell conceptual designs
Rotor-hub bending moment measurements on hingeless rotor helicopter during abrupt maneuvers near ground
Gas lubricated bearing system for turbine compressor
Shock and restart control systems with bypass doors and pressure transducers for mixed compression inlets
Fabricability, mechanical properties, and structural efficiency potentials of boron-polymer film layer composites
Bypass control for mixed compression inlets, discussing normal shock and restart control systems utilizing bypass doors and pressure transducers
Lift engine V/STOL configurations low speed characteristics, measuring exhaust reingestion, inlet pressure, engine and airframe effects in wind tunnels
Effects of boundary layer bleed rate and location on performance of axisymmetric inlet designed for Mach 2.5
Design and test performance of Brayton cycle turbine wheel and shaft mount
Performance characteristics of antenna systems for deep space communication
Turboalternator gas bearing system for spacecraft electric power production
Performance of two stage axial flow turbogenerator with gas bearing rotor support system