Rapid decompression hazards after prolonged exposure to 50 per cent oxygen - 50 per cent nitrogen atmosphere.
Rapid decompression hazards after prolonged exposure to 50 per cent oxygen-50 per cent nitrogen atmosphere
DECOMPRESSION SICKNESS↗
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Rapid decompression hazards after prolonged exposure to 50 per cent oxygen - 50 per cent nitrogen atmosphere
Effects on decompression sickness of breathing oxygen or oxygen-nitrogen mixtures prior to rapid decompression and prolonged low pressure
AEROSPACE MEDICINE↗
Tensile Properties of Irradiated Ti-5 Per Cent Al-2.5 Per Cent Sn ELI at Cryogenic Temperatures
Tensile properties of irradiated titanium, aluminum, and tin alloy at cryogenic temperature
Shogan, R. P.↗
Dark matter measurements combining stellar and H i kinematics: 30 per cent 1σ outliers with low dark matter content at 5 R e
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Meng Yang↗
Thermal changes in the mixture of 20 per cent furfuryl alcohol in aniline
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Griffin, D. N.↗
Gage of 6.5 per cent Si-Fe sheet is chemically reduced
Chemical milling process aids the production of 6.5 percent silicon-iron soft magnetic-alloy sheets to very thin gages. Following conventional rolling to safe gage limits, the material is chemically reduced to the desired gage.
Goldman, A.↗
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↗
Effects of continuous exposure of rats to 100 per cent oxygen at 450 mm. Hg for 64 days.
Continuous exposure of rats to 100 percent oxygen at 450 mm Hg for 64 days shows no physiological effects
PHYSIOLOGICAL RESPONSE↗
Lysosomal enzymes in rats exposed to 100 per cent oxygen.
Lysosomal enzymes in rats exposed to 100 percent oxygen to determine possibility of accelerated in vivo lipid peroxidation
LIPID METABOLISM↗
Risk of mortality in interrupted exposure to 100 per cent 02 - role of air vs. lowered po2.
Effect of periods of air breathing during prolonged exposure to pure oxygen in mice
MOUSE↗
Lysosomal enzymes in rats exposed to 100 per cent oxygen.
Pure oxygen effect on activity of lysosomal aryl sufatase in brain, liver and liver tissue homogenates from rats
OXYGEN TOXICITY↗
Utilization and characteristic velocity saving with a small throttleable region about 92.5 per cent thrust for LM powered descent
Utilizing small throttling capability about high thrust region of 92.5 % for lunar module powered descent
Mc Swain, G. G.↗
An X-ray single crystal investigation of iron- rich alloys of iron and aluminum - Phase relations in alloys containing between 14 and 23 at. per cent aluminum
Phase equilibrium of Fe-rich Fe-Al alloys using single crystal X ray diffraction
Epperson, J. E.↗
Aerodynamic characteristics of a large-scale model with a lift fan mounted in a 5 per cent thick triangular wing, including the effects of BLC on the lift fan inlet
Aerodynamic characteristics of large-scale model with lift fan mounted in 5 percent thick triangular wing
Hall, L. P.↗
Analysis of wind tunnel test results for a 9.39-per cent scale model of a VSTOL fighter/attack aircraft. Volume 1: Study overview
The ability of current methodologies to accurately predict the aerodynamic characteristics identified as uncertainties was evaluated for two aircraft configurations. The two wind tunnel models studied horizontal altitude takeoff and landing V/STOL fighter aircraft derivatives.
Lummus, J. R.↗
Analysis of wind tunnel test results for a 9.39-per cent scale model of a VSTOL fighter/attack aircraft. Volume 2: Evaluation of prediction methodologies
An evaluation of current prediction methodologies to estimate the aerodynamic uncertainties identified for the E205 configuration is presented. This evaluation was accomplished by comparing predicted and wind tunnel test data in three major categories: untrimmed longitudinal aerodynamics; trimmed longitudinal aerodynamics; and lateral-directional aerodynamic characteristics.
Lummus, J. R.↗
Analysis of wind tunnel test results for a 9.39-per cent scale model of a VSTOL fighter/attack aircraft. Volume 3: Effects of configuration variations from baseline
The aerodynamic characteristics of the components of the baseline E205 configuration is presented. Geometric variations from the baseline E205 configuration are also given including a matrix of conrad longitudinal locations and strake shapes.
Lummus, J. R.↗
Analysis of wind tunnel test results for a 9.39-per cent scale model of a VSTOL fighter/attack aircraft. Volume 4: RALS R104 aerodynamic characteristics and comparisons with E205 configuration aerodynamic characteristics
The longitudinal and lateral-directional aerodynamic characteristics of the RALS R104 wind tunnel model are summarized. Configurations for the E205 are also presented for comparison.
Lummus, J. R.↗