Parametric study of a low-density charring ablator
Influence of environmental conditions on thermal performance of low density charring ablator
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Influence of environmental conditions on thermal performance of low density charring ablator
Axial flow compressor study to increase pressure ratio and reduce overall length
Pulmonary pathological response data on four subjects after breathing conditioned atmosphere and being centrifuged
Design parameters for developing phased array acquisition and tracking radar for onboard experiment in Apollo spacecraft
Design parameters influence on size, mass, and reliability of thermionic reactors for electric propulsion
Technical analyses and computer programs in support of optimization of liquid hydrogen thermal protection systems for nuclear Mars spacecraft
Data tables for optimal thermal protection of liquid hydrogen storage in nuclear interplanetary spacecraft
Summary of methodology and results of study of space power systems
Computer program for analysis of space power systems
Numerical solution of coupled, nonlinear, equation of motion for rigid blade to simulate response sensitivity and blade-motion stability of fully articulated rotor
Large area solar array structural design and performance test relationships
Determination of time-temperature-vacuum relationships for sterilization of terrestrial spores
Performance estimates of high speed peripheral jet nuclear powered ground effects machine
Plasma sheath-boundary interactions, analyzing emission, reflection and surface ionization effects on current densities and heat fluxes for cesium and argon
Mars lander thermal control system design parameters including environment, power duty cycle and lander size and weight
Nuclear powered surface effects machine performance estimates, calculating reactor power and payload fraction for various clearance heights, gross weights and velocities
Monte Carlo method for obtaining histogram of distribution of minimum fuel midcourse velocity correction of Venus-72 mission
Analysis of frangible-tube energy absorption system for protection of nuclear aircraft reactor