Animal restraint - Application in space /weightless/ environment
Chicken lymphopenia and body mass loss resulting in death from chronic restraint, developing physiologically unstressful restraint for space environmental testing
Beljan, J. R.↗
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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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Fluid slip ring transfers coolant to rotating equipment
Rotating fluid coupler, consisting of rotor and housing made of aluminum, that is concentric with electrical slip-ring assembly, transfers cooling fluid to instrumentation undergoing environmental tests on rotating platform. Rotating fluid coupler permits unlimited platform revolutions and eliminates danger of lines being pulled loose from supplies.
Mains, D. K.↗
Study to establish criteria for a solar cell array for use as a primary power source for a lunar-based water electrolysis system, phase 3 Final technical report, 15 Nov. 1969 - 15 Dec. 1970
Environmental testing of silicon cell spalling and experimental confirmation of mathematical model
Boretz, J. E.↗
Apollo RCS positive expulsion tankage product improvement program. Task F - Integration and verification of solutions Final report, Jul. 1967 - Sep. 1969
Environmental tests of design modifications for Apollo RCS positive expulsion tankage
Source record↗
Vibration in V/STOL aircraft
Environmental tests of V/STOL vibration effects on human comfort
Jones, W. L.↗
Experimental evaluation of the electrical subsystem of the 2 to 15 kW Brayton power conversion system
Environmental tests of electrical subsystem of 2-to-15 kW Brayton power conversion system
Secunde, R. R.↗
Mariner 71 batteries
Environmental testing and handling of batteries for Mariner 71 spacecraft
Bogner, S.↗
Control moment gyro for Skylab
Skylab control moment gyroscope inner gimbal design and thermal vacuum and environmental tests
Fikes, E. H.↗
Investigation of multilayer printed circuit board materials
Fabrication and environmental tests of circuit boards with polyimide plastic dielectrics and pyrolyzed polyacrylonitrile conductors
Meinhard, J. E.↗
Evaluation of metallic positive expulsion bellows operating parameters with cryogenic propellants
Environmental tests of cryogenic propellant effects on metallic positive expulsion bellows operating parameters
Lange, R. L.↗
MOS capacitors as micrometeoroid detectors
MOS capacitors as low mass micrometeoroid detectors in near-earth space, discussing fabrication and environmental tests
Donovan, R. P.↗
A rugged, stable, differential platinum resistance thermometer
Rugged stable differential Pt resistance thermometer for Lunar Heat Flow Program, discussing construction, calibration and environmental test
Felsenthal, P.↗
A conversational language for the computer- controlled vibration laboratory
User-oriented conversational language computer program for Jet Propulsion Laboratory digital control random excitation environmental test system for spacecraft
Chapman, C. P.↗
Description and applications of a computer program for the interpretation of RGA mass spectra
Computer program for interpretation of residual gas analyzer mass spectra, considering vacuum environmental testing of spacecraft
Babst, R. W.↗
Lubrication of a spacecraft mechanism using the transfer film technique
Nimbus B-2 satellite-borne IR spectrometer lubrication using solid film technique, discussing real time and accelerated vacuum environmental tests
Smith, G. R.↗
SERT 2 gimbal system
The gimbal system is described that was designed to mount the thruster and to reposition the thrust vector of a mercury ion bombardment thruster through the center of gravity of the SERT 2 assembly. The SERT 2 assembly was launched 3 February 1970. The gimbal ring, gimbal mounts, bearings, actuators, and environmental testing are described. Due to the accurate alinements provided, it was not necessary to use the gimbal for the intended function. However, the gimbals were operated successfully numerous times in space after 8 months of storage.
Zavesky, R. J.↗
Development of a space stable thermal control coatings for use in large space vehicles
The preparation and evaluation of zinc orthotitanate and of several new pigments and the environmental testing and evaluation of these pigments and of coatings made from them constitute the bulk of the work accomplished. New pigments were prepared and EPR spectra of pigments and their precursor compounds studied. Results of extensive testing of commercially-available, strippable, protective coatings are reported; Owens-Illinois 650 glass resin has been stabilized against progressive mechanical failures; and definite improvements have been noted. A zinc oxide pigmented lithium silicate paint has demonstrated very good ultraviolet stability.
Gilligan, J. E.↗