Investigation of hydrotest failure of Thiokol Chemical Corporation 260-inch-diameter SL-1 motor case
Hydrotest failure analysis of arc welded, solid propellant rocket motor case
FAILURE MODE↗
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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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Aerodynamic data on a large semispan tilting wing with 0.5-diameter chord, double-slotted flap, and both left-hand and right-hand rotation of a single propeller
Longitudinal aerodynamic data on large-scale semispan V/STOL tilt-wing configuration having single propeller with left and right hand rotation
AERODYNAMIC CHARACTERISTICS↗
Development of a 425 Foot Diameter Passive Communication Satellite with Self Erecting Properties Monthly Progress Report No. 21m, Feb. 1966
Processing equipment modifications and product development of glass fibers for passive communication satellite
PASSIVE SATELLITE↗
A 5-centimeter-diameter electron-bombardment thrustor with permanent magnets
Permanent magnet electron bombardment ion thrustor for station keeping and attitude control of synchronous satellite
ELECTRON BOMBARDMENT↗
Heat transfer from large diameter Pirani gauges operating down to a microtorr
Heat transfer from cylinder in symmetrical chamber resembling Pirani type pressure gauge studied for dependence on pressure, size and temperature of cylinder, and molecular weight of gas
CYLINDER↗
Test of a large-diameter ring-stiffened cylinder subjected to hydrostatic pressure
Buckling test of ring-stiffened cylinder subjected to hydrostatic pressure
BUCKLING↗
Combustion of gaseous hydrogen at low pressures in a 35 deg sector of a 28-inch-diameter ramjet combustor
Shrouded fuel injector for low pressure hydrogen combustion in high-altitude ramjet engine
HYDROGEN FUEL↗
Aerodynamic data on a large semispan tilting wing with a 0.5-diameter chord, a double-slotted flap, and left-hand and right-hand rotation of a single propeller, in presence of fuselage
Aerodynamic characteristics of large semispan tilting wing model having double-slotted flap, rotating propeller, and fuselage
ROTOR BLADE↗
Bending tests of two large-diameter corrugated cylinders with eccentric ring stiffeners
Bending tests of aluminum-alloy corrugated cylinders with eccentric ring stiffeners
CORRUGATED SHELL↗
Development of a 425 foot diameter passive communication satellite with self-erecting properties Quarterly progress report no. 9
Flexure rigidity and tensile strength of Dacron- glass yarn and fiberglass
DACRON↗
Rigidization of a 1.52-meter diameter inflatable solar concentrator in vacuum with associated material studies and fabrication techniques Final report
Foam rigidizing for inflatable paraboloidal solar collector
FOAMED MATERIAL↗
Eighteen-inch diameter expulsion diaphragms Final report
Eighteen-inch expulsion diaphragm recycleability and fabrication from stainless steel and titanium
DIAPHRAGM↗
Aerodynamic data on a large semispan tilting wing with a 0.5-diameter chord, a single slotted flap and both left-hand and right-hand rotation of a single propeller
Longitudinal aerodynamic characteristics of large semispan V/STOL tilt-wing configuration with single propeller rotating in both left and right directions
SEMISPAN MODEL↗
Nondestructive testing of small-diameter refractory alloy tubing
Nondestructive testing methods to evaluate refractory-metal alloy tubing for nuclear application
TUBING↗
Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.19 chord below wing
Wind tunnel tests to determine longitudinal aerodynamic characteristics of large scale semispan V/STOL tilt-wing configuration with single propeller
V/STOL AIRCRAFT↗
Experimental evaluation of high-purity-silica reinforced ablative composites as nozzle sections of 7.8-inch-/19.8 CM/ diameter throat storable-propellant rocket engine
High purity silica reinforced ablative composite materials evaluated as nozzle sections of throat storable propellant rocket engine - erosion rates and charring
SILICON OXIDE↗
Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wing
Longitudinal aerodynamic characteristics of large scale semispan V/STOL tilt-wing configuration having single propeller
AERODYNAMIC CHARACTERISTICS↗
Flight test of a 30-foot nominal diameter disk-gap-band parachute deployed at a Mach number of 1.56 and a dynamic pressure of 11.4 pounds per square foot
Flight test of disk-gap band parachute deployed at low supersonic speed and low dynamic pressure to obtain performance data on planetary entry parachute configurations
SUPERSONIC SPEED↗