Atmospheric collection at 130,000 feet
Atmospheric collection of microorganisms using small biological sampler in upper atmosphere
SAMPLING DEVICE↗
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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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Free-flight measurements of stagnation-point convective heat transfer at velocities to 41,000 ft/sec
Free flight measurements of stagnation point convective heat transfer in air at hypersonic speeds
HYPERSONIC SPEED↗
Extraterrestrial noise in the uhf region /300-3,000 mc/ /noise from the moon/
Thermal radiation and noise measurements from moon
NOISE MEASUREMENT↗
Modular optical test instrument for 1700-11,000 angstrom units.
Optical measuring instrument consisting of eight modular units, specimen chamber and carriage
OPTICAL INSTRUMENT↗
The effect on higher nervous activity of dogs of acute hypoxemia produced by rarefaction of the atmosphere to an altitude of 18,000 meters
Conditioned response behavior of dogs under acute hypoxia
CONDITIONED RESPONSE↗
Penetration of polyethylene into semi-infinite 2024-T351 aluminum up to velocities of 37,000 feet per second
Light gas projector used in penetration of polyethelene into semiinfinite aluminum
LIGHT GAS PROJECTOR↗
Smithsonian Astrophysical Observatory Star Catalog. Positions and Proper Motions of 258,997 Stars for the Epoch and Equinox of 1950.0 Part 1 - Stars 000-001 - 073-708 /bands Plus80deg to Plus30deg/
Ephemeris giving positions and proper motions of 258,997 stellar celestial bodies for epoch and equinox of 1950.0, part I
STAR↗
Development and testing of the disk-gap-band parachute used for low dynamic pressure applications at ejection altitudes at or above 200,000 feet
Development and flight test of inflatable disk- gap-band parachute for high altitude deployment from sounding rockets
SOUNDING ROCKET↗
A report of the physiological, psychological, and bacteriological aspects of 20 days in full pressure suits, 20 days at 27,000 feet on 100 percent oxygen, and 34 days of confinement, part I
Physiological, psychological, and bacteriological aspects of 20 days in full pressure suits in 100 percent oxygen environment
SPACECRAFT ENVIRONMENT↗
A report of the physiological, psychological, and bacteriological aspects of 20 days in full pressure suits, 20 days at 27,000 feet on 100 per cent oxygen, and 34 days of confinement, part III Final report, 2 Jun. 1964 - Nov. 1965
Physiological, psychological, and bacteriological aspects of 20 days in full pressure suits, 20 days at 27.000 feet on 100 percent oxygen, and 34 days of confinement
PSYCHOLOGICAL EFFECT↗
Analysis of vaporization of liquid uranium, metal, and carbon systems at 9000 deg and 10,000 deg R
Vaporization analysis of liquid uranium, metal, and carbon systems at 9000 and 10000 deg R
CARBON↗
High-resolution experimental spectra and theoretical studies of equilibrium radiation from a blunt body traveling at 37,000 ft/sec.
High resolution equilibrium radiation spectra for shock layer of blunt bodies at reentry velocities and radiative recombination of N and O ions
HIGH TEMPERATURE AIR↗
Thermal conductivity of hydrogen from 2,000 deg to 4,700 deg F.
Thermal conductivity of hydrogen at temperatures up to 4700 degrees F determined indirectly from effective conductivity of porous tungsten specimens filled with pressurized hydrogen
TUNGSTEN↗
Direct observations of solar plasma streams at a distance of some 1,900,000 km from the earth, made on february 17, 1961, simultaneous observations of the geomagnetic field pryamyye nablyudeniya potokov solnechnoy plazmy na rasstoyanii poryadka 1 900
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Balandina, S. M.↗
Study made of pneumatic high pressure piping materials /10,000 psi/
Evaluations of five types of steel for use in high pressure pneumatic piping systems include tests for impact strength, tensile and yield strengths, elongation and reduction in area, field weldability, and cost. One type, AISI 4615, was selected as most advantageous for extensive use in future flight vehicles.
Loeb, M. B.↗
The effect of several injector face baffle configurations on screech in a 20,000-pound thrust hydrogen-oxygen rocket
Effects of injector face baffle configurations on screech in hydrogen-oxygen rocket engine
INJECTOR↗
Global behavior of the ionosphere at 1,000 kilometers altitude
Satellite measurements of electron temperature and concentration in ionosphere behavior studies
ELECTRON TEMPERATURE↗
Momentum Transfer and Cratering Phenomena Associated With the Impact of Aluminum Spheres Into Thick Aluminum Targets at Velocities to 24,000 Feet Per Second
Spheres of 2017-T4 aluminum with diameters of, 1/16, 1/8, and ½ inch were launched into semi-infinite targets of 2024-T4 and 1100-0 aluminum. The momentum transfer during impact was measured by means of a simple ballistic pendulum to which the target was attached. The ratio of target momentum to projectile momentum increased with increasing projectile velocity and with projectile diameter. Mass loss due to cratering, penetration, and crater diameter were also obtained for these experiments. It was noted that the variation of these parameters was also a function of the projectile diameter. No conclusive evidence was uncovered to explain this apparent scale effect. However, close examination of the various craters suggests that the cratering process is, in fact, different for the different size projectiles. The cause for this difference has yet to be resolved.
MOMENTUM TRANSFER↗