Experimental evaluation of six ablative-material thrust chambers as components of storable-propellant rocket engines
Test firing evaluation of six ablative-material thrust chambers as components of storable propellant rocket engines
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Test firing evaluation of six ablative-material thrust chambers as components of storable propellant rocket engines
Design modifications for six converter solar thermionic generator
Aerobee rocket sounding of far UV spectra of six stars in Orion, extrapolating mass ejection from resonance absorption lines
Hypotheses and estimation of correlation coefficient using six and eight quantiles, with application to space telemetry
Six converter solar thermionic generator
Optimization of VTOL control concepts and comparison on six degree of freedom motion simulator
Description and performance analysis of manned six-pass orbital mission /Mercury-Atlas 8/
Optimization of VTOL control concepts with and without stabilization compared with six degree of freedom motion simulator, noting system failure effects and nonlinear concepts
Thirty-six element square array, with mutual coupling between crossed slots for array elements, is used as an electronically scanned tracking antenna. The system does not require the movement of the antenna or the presence of an operator.
Six converter solar thermionic generator
Major solar and solar-induced phenomena during 20th solar cycle, first six months, 1967
Computer simulation of six degree of freedom flight equations
Stellar photometric data for six photocathode materials and silicon detector
Evaluation of six degrees of freedom motion simulator for Bell X-14A aircraft hovering characteristics
Computer solution of six degrees of freedom flight equations, discussing advantages of using flight path axes for translational equations of motion
Electrical testing of six converter solar energy thermionic generator, discussing overheating and dual current mode anomalies
Induced interference effects on aerodynamic characteristics of 0.16-scale six-jet V/STOL model in transition
Wind tunnel tests of V/STOL transport model with six wing mounted lift fans