R and D and evaluation of a lightweight, high strength magnesium alloy Quarterly report, 1 Aug. - 1 Nov. 1968
Preparation, casting, and extruding lightweight, high strength magnesium-scandium alloy
Foerster, G. S.↗
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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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Fabrication and test of lightweight honeycomb sandwich structures Final report
Fabrication and testing of lightweight honeycomb sandwich structures
Dawson, J. E.↗
A flight investigation of a lightweight helicopter to study the feasibility of fixed-collective-pitch autorotations
Flight investigation of lightweight helicopter to study feasibility of fixed collective pitch autorotations
Pegg, R. J.↗
Development of lightweight solar panels Summary report, Jan. 1966 - Mar. 1969
Fabrication and test evaluation of lightweight solar panels
Carlson, J. A.↗
Development of an integrated lightweight flexible silicon solar cell array Quarterly technical report, 1 Jul. - 1 Oct. 1969
Design criteria for integrated lightweight flexible silicon solar cell arrays
Ralph, E. L.↗
Lightweight large area solar arrays.
Lightweight large area solar cell arrays for space programs with multikilowatt predicted performance, noting rollup array orbital flight testing
Abbott, D. D.↗
Lightweight S-band helix antenna
Pyrotechnically operated S-band helical antenna is developed in which helix is deployed subsequent to antenna placement. Antenna is small, lightweight, and novel in that deployable helix is used in place of fixed dish or horn. It can be designed to cover L- and X-band frequencies.
Cribb, H. E.↗
R and D evaluation of a lightweight, high strength magnesium alloy Quarterly report, 1 May - 1 Aug. 1969
Lightweight, high strength magnesium alloy development with magnesium-scandium-lithium selection
Foerster, G. S.↗
Development of an integrated lightweight flexible silicon solar cell array Quarterly technical report, 1 Oct. 1969 - 1 Jan. 1970
Technical progress in program to develop integrated lightweight flexible silicon solar cell array
Ralph, E. L.↗
The design study of a lightweight rotor hub for a Mars-landing autogyro
Lightweight rotor hub design for Mars landing autogyro
Rayfield, W. P.↗
Vacuum leakage tests of a simulated lightweight spacecraft air lock
Structural sealing problems and leakage rates of lightweight simulated spacecraft air lock under high vacuum
Trout, O. F., Jr.↗
Air permeability studies of a lightweight coated fabric subjected to uniaxial tensile loads with and without prior cycling
Air permeability of lightweight fluorcarbon rubber-coated high temperature Nylon fabric under uniaxial tensile loads at room temperature
Deaton, J. W.↗
Lightweight mirror structures
Borosilicate glass and monolithic core technology for lightweight astronomical mirror construction
Loytty, E. Y.↗
Self-weight loaded structures in the context of lightweight mirror applications
Structural analysis for optimal load carrying substrate members of lightweight astronomical mirror
Duncan, J. P.↗
Development of an integrated lightweight flexible silicon solar cell array Final report
Methods and analytical techniques for fabricating integrated lightweight flexible silicon solar array blanket
Ralph, E. L.↗
Development of an integrated lightweight flexible silicon solar cell array Final report
Development of integrated lightweight flexible silicon solar cell array
Ralph, E. L.↗
A DTA-EGA experiment for a lightweight Martian landed capsule
Differential thermal analysis-effluent gas analysis /DTA-EGA/ experiment for lightweight Martian landed capsule
Bollin, E. M.↗
Operation of a lightweight power conditioner with a hollow cathode ion thruster
Hollow cathode ion thrustor and lightweight power conditioner of solar-electric propulsion system for unmanned deep space probes
Costogue, E. N.↗