Lubrication and bearing problems in the vacuum of space.
Lubrication and bearing problems in space environment, noting molybdenum disulfide and silicones
SPACE ENVIRONMENTAL LUBRICATION↗
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Results for “e+-e−”
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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Flight results with a non-aerodynamic, variable stability, flying platform.
Research and operational results obtained with nonaerodynamic variable stability flying platform for examining problem associated with lunar landing
ATTITUDE CONTROL↗
B and C ''sources'' of Jovian decametric radiation.
Short duration pulses association with subsidiary B and C sources of Jovian decametric radiation
RADIO SOURCE↗
An assessment of ground and flight simulators for the examination of manned lunar landing.
Free flying lunar landing research vehicle tested for more than two years and used in lunar landing simulations supporting Apollo project
APOLLO PROJECT↗
Nose selection and vehicle motion dynamics for the second stage of a two-stage sounding rocket system.
Nose selection and vehicle motion dynamics for second stage of two-stage sounding rocket system, discussing nose shapes effect on altitude performance, overall vehicle stability, bending moments, etc
TWO-STAGE ROCKET↗
Observations of an infrared star in the Orion nebula.
IR star in Orion nebula noting photometric result, comparing IR flux with energy distribution of black body as function of wavelength
INFRARED ASTRONOMY↗
Lunar Orbiter camera.
Dual camera for Lunar Orbiter, design, performance and hardware modifications
LUNAR ORBITER↗
The positions and angular extent of OH EMISSION associated with the H II regions W3, W24, W49, and NGC 6334.
OH emission regions investigated using Millstone and Haystack antennas with interferometer, noting radio sources for base-line calibration and instrumental phase monitoring
RADIO ASTRONOMY↗
Determination of Mars atmospheric composition by shock-layer radiometry during a probe experiment.
Mars atmospheric composition determination by shock layer radiometry technique during probe experiment
MARS ATMOSPHERE↗
Observations of OH emission in the H II REGION W3 with a 74400 lambda interferometer.
OH emission in H II region W3, using improved equipment
HYDROXYL↗
Measured effects of various combinations of nuclear radiation, vacuum, and cryotemperatures on aerospace adhesives.
Adhesives for nuclear powered spacecraft tested for pressure, temperature and radiation effects
VACUUM EFFECT↗
The performance of glass filament-wound pressure vessels with metal liners at cryogenic temperatures.
Metal lined glass filament-wound pressure vessel performance at cryogenic temperatures, discussing fibers, resins and liners
PRESSURE VESSEL↗
Theoretical high-pressure equations of state including correlation energy.
High pressure equations of state including electron gas correlation energy, giving density vs pressure curves for various elements
CORRELATION FUNCTION↗
Spectral line interferometry with independent time standards at stations separated by 845 kilometers.
Upper limit of arc for hydroxyl /OH/ emission region associated with radio source W3, using Michelson interferometer consisting of two spaced radio telescope stations
RADIO TELESCOPE↗
The galactic radio source W49 at 3.4 mm.
Galactic radio source W49 at 3.4 mm, showing no additional components in spectrum with turnover points at various frequency ranges
GALACTIC RADIO WAVE↗
Calculation of molecular band spectra assuming a Gaussian line profile.
Moleuclar band spectra of CN emission assuming Gaussian rotational line profile
SPECTRAL BAND↗
On panel vibration damping due to structural joints
Explore the source record for details and available documents.
Carbonell, J. R.↗
Analysis of filament reinforced metal-shell pressure vessels
Computer program analyzes design requirements and computes designs for metal-lined filament-wound pressure vessels with either geodesic /helical/ or in-plane filament winding patterns on the cylindrical portion and over the ends, reinforced by circumferential windings on the cylindrical portion.
Landes, R. E.↗