Full scale flight test report, X-15A-2 ablative thermal protection system
Flight test and performance analysis of ablative thermal protection system for X-15A-2 aircraft
Price, A. B.↗
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Results for “Performance analysis”
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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First U.S. manned six-pass orbital mission /Mercury-Atlas 8, spacecraft 16/
Description and performance analysis of manned six-pass orbital mission /Mercury-Atlas 8/
Boynton, J. H.↗
Surveyor 6 mission report. Part 1 - Mission description and performance
Mission description and postflight performance analysis of Surveyor 6 spacecraft
Source record↗
Advanced converter development.
Thermal and performance analysis for thermionic converters with rhenium and palladium collectors, noting emitter-temperature errors
Brosens, P. J.↗
Theoretical study of antenna problems in radio astronomy Final report, 1 Jul. 1963 - 1 Sep. 1967
Performance analysis on satellite borne traveling wave antenna for low frequency signal detection
Sandler, S. S.↗
Theoretical analyses of electrothermal thrusters with supersonic heat addition.
Performance analysis for electrothermal thrustor using lithium propellant with supersonic heat addition
Leon, H. I.↗
Solid propellant engineering
Heat transfer and combustion termination of solid propellants, and solid propellant propulsion system performance analysis
Source record↗
Apollo 9 LM-3 ascent propulsion system, final flight evaluation
Steady state performance analysis for ascent propulsion system during Apollo 9 mission burn to depletion
Griffin, W. G.↗
User's Manual for Computer Program HEPCAT
HEPCAT computer program for rocket engine test data reduction and performance analysis - users manual
Garza, C. C.↗
Space shuttle booster return performance
Space shuttle booster entry and subsonic performance analysis
Bithell, R. A.↗
Comparative performance of double focused and quadrupole mass spectrometers
Comparative performance analysis of double focused and quadrupole mass spectrometers
Wilson, S. K.↗
Theoretical analyses of electrothermal thrusters with supersonic heat addition
Performance analysis for electrothermal thrustor using lithium propellant with supersonic heat addition
Leon, H. I.↗
Apollo 11 laser ranging retro-reflector - Initial measurements from the McDonald Observatory
Apollo 11 laser ranging retro reflector measurements from McDonald Observatory confirming thermal design analysis performance prediction
Alley, C. O.↗
Thermal and performance analyses of the orbital workshop solar array system
Saturn IB Orbital Workshop solar array thermal and performance analysis for various vehicle orientations and orbital conditions, emphasizing modeling and data handling
Simmons, C. W.↗
Technical, analytical, and computer support Annual report, 18 Feb. 1970 - 17 Feb. 1971
Design study with mathematical model for performance analysis of silicon-germanium thermoelectric generators
Source record↗
Skylab 1 NASTRAN Stress Analysis Models
NASTRAN computer program applications in stress analysis performed on Skylab hardware
Viall, W. S.↗
Oscillating hot-wire anemometer
Performance analysis was made of oscillating hot-wire anemometer electrical output in gas stream. Advantages include no calibration and measurement of fluid direction as well as fluid speed.
Conley, J. M.↗
Wind-tunnel simulation of store jettison with the aid of magnetic artificial gravity
A method employed in the simulation of jettison of stores from aircraft involving small scale wind-tunnel drop tests from a model of the parent aircraft is described. Proper scaling of such experiments generally dictates that the gravitational acceleration should ideally be a test variable. A method of introducing a controllable artificial component of gravity by magnetic means has been proposed. The use of a magnetic artificial gravity facility based upon this idea, in conjunction with small scale wind-tunnel drop tests, would improve the accuracy of simulation. A review of the scaling laws as they apply to the design of such a facility is presented. The design constraints involved in the integration of such a facility with a wind tunnel are defined. A detailed performance analysis procedure applicable to such a facility is developed. A practical magnet configuration is defined which is capable of controlling the strength and orientation of the magnetic artificial gravity field in the vertical plane, thereby allowing simulation of store jettison from a diving or climbing aircraft. The factors involved in the choice between continuous or intermittent operation of the facility, and the use of normal or superconducting magnets, are defined.
Stephens, T.↗