Performance of a 16.6-meter-diameter cross parachute in a simulated Martian environment
Inflation and drag characteristics of cross parachute in simulated Martian environment
Coltrane, L. C.↗
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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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Dynamic stability of a 4.6-meter-diameter 120 deg conical spacecraft at Mach numbers from 0.78 to 0.48 in a simulated Martian environment
Subsonic dynamic stability characteristics of large conical spacecraft in simulated Martian environment
Bendura, R. J.↗
Lunar radar scattering at 6 and 12 meter wavelengths
Lunar radar echoes at 6 and 12 m wavelengths analyzed to obtain lunar surface scattering data
Burns, A. A.↗
Wind tower influence study /For NASA's 150-meter meteorological tower at Kennedy Space Center, Florida/
Analytical and experimental study of effects of 150 m meteorological tower structure on wind measurements
Hathorn, J. W.↗
Characteristics of turbulence observed at the NASA 150-meter meteorological tower.
Design data for launch vehicle ground wind response obtained from 150-m meteorological tower turbulence characteristics
Fichtl, G. H.↗
Meteorological measuring and recording equipment description, calibration, and maintenance procedures for nasa's 150 meter meteorological tower facility, kennedy space center, florida
Explore the source record for details and available documents.
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Mercury cadmium telluride as a 1- to 20- micro-meter wavelength infrared detector for space applications
Mercury cadmium telluride as 1- to 20-micrometer wavelength infrared detector for space applications
Packard, R. D.↗
Real-gas effects in critical flow through nozzles and thermodynamic properties of nitrogen and helium at pressures to 300 times 10 sup 5. Newtons per square meter /approx. 300 ATM/
FORTRAN 4 subroutines for calculating critical flow factor to determine mass flow rate of gaseous helium and nitrogen through critical flow nozzles
Johnson, R. C.↗
A bonding material for optically immersing infrared detectors from 2 to 14 micro-meters
Visible and infrared transmitting properties of epoxy resin suitable for infrared detectors
Packard, R. D.↗
Flight-test results from supersonic deployment of an 18-foot-diameter /5.49 meter/ towed ballute decelerator
Supersonic deployment and extraction of inflatable towed ballute decelerator
Eckstrom, C. V.↗
Performance, systems designs, modifications, radiometry, operational problems, and corrective procedures associated with a 1.75 meter off-axis solar simulator
Solar simulator design and performance characteristics
Duncan, C. H.↗
Directional Doppler bloodflow meter Progress report
Ultrasonic blood flowmeter using Doppler effect in acoustic scattering from moving corpuscles
Mc Leod, F. D.↗
Gaseous hydrogen requirements for the discharge of liquid hydrogen from a 1.52 meter /5 ft/ diameter spherical tank
Physical parameter effect on pressurant gas requirements during expulsion of liquid hydrogen from spherical tanks
Dewitt, R. L.↗
Gaseous-Hydrogen Pressurant Requirements for the Discharge of Liquid Hydrogen from a 3.96 Meter /13 ft/ Diameter Spherical Tank
Hydrogen gas pressure requirements during pressurization and transfer of liquid hydrogen from spherical tanks
Stochl, Robert J.↗
Investigation of the turbulent wind field below 150-meter altitude at the eastern test range
Statistical effects of wind and atmospheric turbulence on launch vehicles
Blackadar, A. K.↗
Hall effect transducer gives electrical output proportional to meter shaft rotation
Electrical output transducer for measuring angular displacements does not introduce frictional contact between stationary and moving parts. It produces output voltages directly proportional to small rotary shaft displacements.
Smith, D.↗
Cape Kennedy peak wind profile probabilities for levels from 10 to 150 meters
Peak wind probabilities for atmosphere over Cape Kennedy launching base
Bowman, W. A.↗
Preparation of mirror coatings for the vacuum ultraviolet in a two-meter evaporator
Design and performance of evaporator for vacuum ultraviolet mirror coatings by aluminum compound films
Bradford, A. P.↗