Development of a prototype waste collection system /the Hydro-John/
Characteristics of prototype waste collection system for spacecraft applications
Murray, R. W.↗
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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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Design and development of a prototype System Performance Evaluation Console /SPEC/ Final report, Jun. 1969 - May 1970
Design of prototype systems performance evaluation console as man machine interface
Thompson, R. W.↗
Development of a prototype onboard EEG analysis system
Laboratory prototype system for acquisition, automatic analysis, and display of astronaut electroencephalographic and electro-oculographic signals, and spacecraft noise effects on sleep
Frost, J. D., Jr.↗
Space shuttle structural prototype design, fabrication, and test
Space shuttle structural prototype design, fabrication and test program
Engler, E. E.↗
Prototype of a new lunar-gravity simulator for astronaut mobility studies.
Prototype lunar gravity simulator for studies of reduced gravity effects on human self locomotive capability, using magnetic air bearings and body support system
Spady, A. A., Jr.↗
A prototype cloud physics laser nephelometer
Prototype cloud physics laser nephelometer design and performance, determining droplet concentration and size from scattered light pulse count and amplitudes
Blau, H. H., Jr.↗
Prototype electrolyzer for oxygen generation from water vapor
Prototype electrolyzer for generating oxygen from water vapor under various atmospheric conditions, noting spacecraft cabin application
Smith, E. L.↗
Functional and physical design of a flight prototype ion engine power conditioner
Space compatible flight prototype ion engine power conditioning system design for Hg thrustor using oxide cathode
Benson, G. C.↗
Flight prototype electrostatic ballastic pendulum Final report
Flight prototype electrostatic ballistic pendulum momentum transducer
Powell, J. G.↗
Prototype airborne one-third octave band spectrum analyzer for acoustic and vibration data
Design and test evaluation of prototype one-third octave band spectrum analyzer for measurement and analysis of acoustic and vibration data onboard space vehicles
Source record↗
Development and test of a flight prototype power conditioner for 20 cm mercury bombardment electric thruster system
Development and tests of flight prototype power conditioner for 20 cm mercury bombardment electric thruster system
Source record↗
Development of a prototype waste collection system /the modified Hydro John/
Development of prototype waste collection system /modified Hydro John/ designed for use in either zero or one gravity environment
Mangialardi, J. K.↗
Development and testing of a prototype operational system for automatic monitoring of sleep during manned space flight Final report
Prototype device for monitoring sleep during manned space flight including performance tests
Frost, J. D.↗
Design, fabrication, and preliminary evaluation of thermal and hydraulic performance of a prototype SNAP-8 mercury boiler
Thermal and hydraulic performance of prototype SNAP-8 mercury boiler - design, fabrication, and preliminary evaluation
Furman, E. R.↗
Design and development of a prototype static cryogenic heat transfer system
Design and development of prototype static cryogenic heat transfer system utilizing heat pipe with wetting arterial wick and nitrogen as working fluid
Source record↗
Design and fabrication of a flight-concept prototype electrochemical water recovery subsystem
Design and fabrication of flight-concept prototype electrochemical water recovery subsystem
Putnam, D. F.↗
System features of a space station prototype environmental thermal control and life support system
Space station prototype environmental thermal control and life support systems, considering maintainability, reliability, weight penalties and fault detection and isolation
Flugel, C.↗
Validation of SERT 2 thermal analytical techniques by thermal vacuum testing of the prototype satellite
The thermal protection system for the flight configuration of the SERT 2 satellite was designed using an analytical thermal network to represent the satellite and its environment. A large part of this digital analytical network was adjusted and calibrated by comparing predicted temperatures with experimental measurements made with the prototype SERT 2 satellite in an extended thermal vacuum test. The procedures used in adjusting and calibrating the analytical network are outlined.
Smolak, G. R.↗