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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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At least 487 records · Page 27

All sources NASA NTRS DOE OSTI

NASA NTRS1963

SEMITHEORETICAL CONSIDERATION ON SCALING LAWS IN FLAME STABILIZATION

Scaling laws in stability of flames on flameholder

SCALING LAW↗

NASA NTRS1963

THEORETICAL CONSIDERATIONS FOR A PRELIMINARY DESIGN OF A SOLAR CELL GENERATOR ON A SATELLITE

Solar cell generators for satellite power supply - design theory

SOLAR CELL↗

NASA NTRS1963

EARTH ORBITING SPACE STATIONS- CONFIGURATIONS AND DESIGN CONSIDERATIONS

Design configurations for orbiting space stations

SPACE STATION↗

NASA NTRS1962

CONSIDERATION ON THE DESIGN OF PFM TELEMETRY ENCODERS

Encoding techniques used in pulse frequency modulation telemetry systems for s-3 and uk-1 satellites

SATELLITE COMMUNICATION↗

NASA NTRS1963

CONSIDERATIONS ON THE EVAPORATION OF MATERIALS IN VACUUM

Development of a standard operating procedure for testing the evaporation of materials in a vacuum, including data on tests of plastics and greases

MATERIAL TESTING↗

NASA NTRS1963

ANALYTIC CONSIDERATIONS RELATED TO THE LEWIS TYPE BOMBARDMENT ION ENGINE

Model for determining regions of weak and strong plasmas, and calculation of radial variation of plasma density and potential

ION ENGINE↗

NASA NTRS1963

PROPELLER WHIRL FLUTTER CONSIDERATIONS FOR V/STOL AIRCRAFT

Propeller whirl flutter conditions peculiar to v/stol aircraft and the related problem of the response of propeller-nacelle system to random atmospheric turbulence

V/STOL AIRCRAFT↗

NASA NTRS1963

OPTICAL ELECTRICAL DESIGN CONSIDERATIONS FOR CONCENTRATING SOLAR CELL PANELS

Optical-electrical design of a concentrating solar cell panel with evaluation of factors affecting its performance and earth space power source

ELECTRO-OPTICS↗

NASA NTRS1963

SOME GENERAL CONSIDERATIONS OF MANNED LUNAR RETURN MISSIONS

Manned lunar return mission planning, discussing the utilization of one space vehicle or two for the lunar orbit rendezvous and return phases

LUNAR FLIGHT↗

NASA NTRS1963

TRAJECTORY AND GUIDANCE CONSIDERATIONS FOR LUNAR RETURN MISSIONS

Problems involved in meeting trajectory and guidance requirements for the return-to-earth and atmospheric reentry of a lunar spacecraft

SPACECRAFT GUIDANCE↗

NASA NTRS1963

TRAJECTORY CONSIDERATIONS FOR THE RETURN TO EARTH PHASE OF LUNAR MISSIONS

Trajectory requirements for lunar injection and earth reentry conditions are considered in the return-to-earth phase of lunar missions

REENTRY TRAJECTORY↗

NASA NTRS1963

MARTIAN ENTRY CAPSULE- DESIGN CONSIDERATIONS FOR TERMINAL DECELERATION

Retardation system for capsule entering martian atmosphere

DESCENT↗

NASA NTRS1945

CONSIDERATIONS IN DESIGN OF CALORIMETERS FOR THE PROJECT FIRE SUPERORBITAL RE-ENTRY TEST VEHICLE

Design of calorimeters to obtain flight data at lunar reentry velocity and equations to convert telemetered temperature responses into heat flux valves

REENTRY EFFECT↗

NASA NTRS1963