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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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Shock tube instrumentation methods for convective heat transfer study and radiative properties of high temperature gas at conditions simulating hypervelocity entry
Shock tube instrumentation to study convective and radiative heat transfer of hot gases simulating hypervelocity reentry
Sonic boom measurement instrumentation noting use of frequency response, vibration isolation, wind screening, etc
A detailed review of the development of instruments for X-ray astronomy is given with major emphasis on nonfocusing high-sensitivity counter techniques used to detect cosmic photons in the energy range between 0.20 and 300 keV. The present status of X-ray astronomy is summarized together with significant results of the Uhuru observations, and photon interactions of importance for the detection of X-rays in space are noted. The three principal devices used in X-ray astronomy (proportional, scintillation, and solid-state counters) are described in detail, data-processing systems for these devices are briefly discussed, and the statistics of nuclear counting as applied to X-ray astronomy is outlined analytically. Effects of the near-earth X-ray environment and atmospheric gamma-ray production on X-ray detection by low-orbit satellites are considered. Several contemporary instruments are described (proportional-counter systems, scintillation-counter telescopes, modulation collimators), and X-ray astronomical satellite missions are tabulated.
Two dimensional airfoil testing was conducted at the Wichita State University Beech Wind Tunnel for a number of years. The instrumentation developed and adapted during this period of testing for determination of flow fields along with traversing mechanisms for these probes are discussed. In addition, some of the techniques used to account for interference effects associated with the apparatus used for this two dimensional testing are presented. The application of a minicomputer to the data reduction and presentation is discussed.
Sensor and calibration techniques for measurement of infrasonic and gravity waves noting error control and possible applications
During high-speed entry and descent through the atmosphere of Mars, the two Viking spacecraft will make in situ measurements of the structure of the atmosphere. The profiles of temperature, pressure, and density with altitude will be defined from an altitude of about 100 km to touchdown, from measurements of the atmospherically induced deceleration and directly measured temperatures and pressures, the latter at altitudes below about 20 km. These data will be supplemented by onboard-radar altitudes and, below 8 km, by three-component Doppler radar velocities. Winds will be derived from the Doppler velocities and from gyro records of vehicle attitude changes. The planet radius at the landing site, needed to interpret the atmospheric data, will be defined to within a few tenths of a kilometer from the measured acceleration due to gravity after landing. It is expected that temperature will be determined to within about 1 K in the lower atmosphere, and to within a few degrees up to 100 km; pressures to within a few percent; and wind velocities to within about 2 meters/second below 8 km.
Velocity measurements in flames and the simultaneous measurement of droplet size and velocity with the aid of laser anemometry are considered along with methods of particle size measurement and techniques based on laser Raman spectroscopy. Attention is given to high-speed photography and holography, computer compensated thermocouples, and the determination of turbulence characteristics. The employment of suction probes is also discussed, taking into account sampling methods, the effects of temperature change in sampling probes on particle formation, and the chemical analysis of samples.
Array failure modes, relevant materials property changes, and primary degradation mechanisms are discussed as a prerequisite to identifying suitable measurement techniques and instruments. Candidate techniques and instruments are identified on the basis of extensive reviews of published and unpublished information. These methods are organized in six measurement categories - chemical, electrical, optical, thermal, mechanical, and other physicals. Using specified evaluation criteria, the most promising techniques and instruments for use in life prediction tests of arrays were selected.
Compilation of electronic test instrumentation and techniques derived from NASA programs
Instrumentation and techniques of torsional pendulum and braid analyses, studying trace moisture and cure cycle effects on thermomechanical spectra of polymeric materials
Techniques and instrumentation for measurements of ultraviolet solar emission spectrum
A general survey is presented of solar radiation measurement, techniques, and instrumentation. The importance of determining the total and spectral irradiance of the sun is examined in the context of the energy crisis and utilization of solar energy. The survey includes the extraterrestrial solar fluxes, their possible variations, problems relating to energy received by collecting surfaces on the ground, major types of instrumentation, and the radiation scales to which the measurements are referred. The type of insolation data available is reviewed. Alternate techniques of deriving insolation data with high space-time resolution are discussed with reference to solar energy conversion requirements. Energy received on the ground can be computed from known values of the extraterrestrial solar spectrum and of the spectral absorption parameters of the atmosphere. Another technique is based on measurements made by meteorological satellites of the cloud-cover and of the solar energy reflected and scattered back to space by the earth-atmosphere system.
The development of techniques and instrumentation suitable for the nondestructive evaluation of purged multilayer insulation prior to and after a shuttle orbiter flight is discussed. These techniques are desirable because of the possibility that corrosion, compression, or tearing of the insulation will degrade the performance of the insulation during subsequent flights. A second objective was the application of the developed technology to the evaluation of other insulation types. Three nondestructive evaluation techniques, electromagnetic, thermal, and acoustic were selected for evaluation. The results of evaluation of each technique are described.
Instrument measures concentration of small particles in aqueous medium in terms of amount of light scattered and degree to which light transmission is attenuated. Sensitivity to small particles is optimized because both scattered and transmitted illumination levels are detected by photodiodes.
Instrumental activation analysis technology for analysis of meteorites and lunar materials
Several methods for aiding acoustic measurements inside wind tunnels are described; these include: placing acoustic material in the test section, using low tip-speed drive fans for reducing background noise, using proper microphone strut design for low wind noise, using directional receivers, and simulating the reverberant noise fields. The instrumentation and techniques were developed for acoustic research in both a small and a large closed-test-section wind tunnel at NASA Ames Research Center, and may be applicable to many different types of aeroacoustic wind tunnels.
Technical information is presented covering the areas of: (1) analytical instrumentation useful in the analysis of physical phenomena; (2) analytical techniques used to determine the performance of materials; and (3) systems and component analyses for design and quality control.