Analytical and experimental study of ablation material for rocket engine application Final report
Techniques for rating performance of ablative materials in liquid-propellant rocket engines
ABLATING MATERIAL↗
SEARCH · Engineering Papers
Results for “ablator”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Development of Ablation Sensors for Advanced Reentry Vehicles
Design and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal parameters of ablative reentry vehicle heat shield
ABLATING MATERIAL↗
Development and fabrication of ablative optical beacons Final report, 4 Dec. 1965 - 30 Apr. 1966
Lifetime, reliability, and radiation spectrum of ablative flash lamp for Apollo command service module
LIFETIME↗
Analytical determination of the effect of thermal property variations on the performance of a charring ablator
Effects of thermal-property variations on performance of charring ablator
ABLATING MATERIAL↗
Analytical study of diffusion-controlled char oxidation and its effect on steady-state ablation of plastic materials
Analytical study of diffusion-controlled char oxidation and effect on steady state ablation of plastic materials
STEADY STATE↗
Exploratory investigation of the effect of nylon grain size on ablation of phenolic nylon
Exploratory investigation of nylon grain size effect on ablation of phenolic nylon
NYLON↗
Preliminary Evaluation of a Number of Ablative Heat-shield Materials Exposed to Combined Radiative and Convective Heating
Ablating materials tested at combined radiative and convective heating for manned reentry vehicle heat shields
REENTRY VEHICLE↗
Investigation of resin systems for improved ablative materials Final report, 19 Jun. 1964 - 31 Jul. 1965
Resin systems investigated for improving ablative materials for use with fluorine-containing liquid propellant systems
LIQUID PROPELLANT↗
Determination of thermophysical properties of ablative materials. Phase I - Laboratory determinations. Part A - Heat capacity, density, decomposition and melt temperature
Laboratory determinations of thermophysical properties of ablative materials
APOLLO SPACECRAFT↗
Apollo afterbody heat transfer and pressure with and without ablation at M infinity of 5.8 to 8.3
Apollo afterbody heat transfer and pressure with and without ablation at Mach numbers 5.8 - 8.3
AFTERBODY↗
Determination of temperature and material effects on high-velocity impact craters in ablative heat-shield materials
Temperature and material effects on high-velocity impact craters in phenolic-nylon and elastomeric ablative heat-shield materials
ABLATING MATERIAL↗
Ablative and insulating properties of outgassed boron nitride and boron nitride composite
Ablative and insulating properties of outgassed boron nitride and boron nitride-phenolic resin composite
ABLATION↗
An experimental evaluation of 100-lb-thrust ablatively cooled rocket engines
Test firing of 100-lb thrust ablatively cooled rocket chambers
ROCKET CHAMBER↗
Development of sensors to obtain in-flight ablation measurements of thermal-protection materials
Design and development of sensors for measuring ablative changes in space vehicle heat shield during reentry phase
ABLATION↗
Thermochemical ablation.
Thermochemical interaction between ablation material and environment during manned reentry, using mainly graphite and composite materials
REENTRY EFFECT↗
Melting ablation about decelerating spherical bodies.
Heat transfer and melting ablation about decelerating spherical bodies during planetary atmosphere entry
REENTRY PHYSICS↗
Evidence of surface waves and spreading of turbulence on ablating models.
Surface modifications of recovered small-scale plastic models after high speed flight used to estimate extent of laminar and turbulent flow over surface related to ablation studies
ABLATING NOSE CONE↗
Experimental investigation of a charring ablative material exposed to combined convective and radiative heating.
Charring ablative materials effectiveness in combined convective and radiative heating as reentry shield
MATERIAL TESTING↗