Heat of pyrolysis of resin in silica-phenolic ablator.
Heat of pyrolysis of resin in silica-phenolic ablator determined from combustion calorimetry measurements of heats of formation
SILICON OXIDE↗
SEARCH · Search NASA
Results for “ABLATION”
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.
Investigation of fiber systems of ablative materials Final report
Reinforcing fiber systems for ablative composite materials - application to thrust chambers of liquid-fuel rocket engines
REINFORCING FIBER↗
Parametric study of a low-density charring ablator
Influence of environmental conditions on thermal performance of low density charring ablator
ENVIRONMENTAL TESTING↗
Analysis of surface ablation of noncharring materials with description of associated computing program
Generalized method, including computer program, to solve problem of heat transfer and material response for stagnation region of blunt bodies experiencing ablation
ABLATION↗
A study of ablation effects on antenna performance Final report, 7 Jul. 1965 - 12 Oct. 1966
Dielectric property screening tests, and temperature range tests for determining ablation material effects on Apollo model antennas - simulation of thermal protection system
ANTENNA↗
Investigation of 3-D fabrication of ablative materials Final report, 8 Sep. 1965 - 18 Oct. 1966
Textile processes evaluated for fabrication of three-dimensionally reinforced ablative materials - thermal, physical, and mechanical properties of fabric composites with epoxy resin
REINFORCED MATERIAL↗
Studies of nozzle ablative material performance for large solid boosters Final report
Carbon phenolic, graphite phenolic, and silica phenolic nozzle ablative materials performance for large solid propellant rocket boosters
NOZZLE EFFICIENCY↗
Convective and radiative heat transfer to an ablating body, part I Final report
Convective and radiative heat transfer to entry vehicles with ablative heat shield
RADIATIVE HEAT TRANSFER↗
Performance of three ablation materials during simulation of long-duration afterbody heating
Resistance to heat penetration and deformations or buckling of three ablation materials during simulated exposure to lifting vehicle afterbody heating
HEAT RESISTANCE↗
A survey of thermal radiation studies of ablating bodies in the ballistic range
Thermal radiation studies of ablating bodies in ballistic range
BALLISTIC RANGE↗
Decomposition characteristics of a char- forming phenolic polymer used for ablative composites
Decomposition characteristics of char-forming phenol formaldehyde polymer used for ablative composites
PHENOL FORMALDEHYDE↗
Effect of thermocouple wire size and configuration on internal temperature measurements in a charring ablator
Thermocouple wire size and configuration effects on internal temperature measurements in charring ablator
ABLATING MATERIAL↗
Boundary-layer separation and reattachment with and without ablation
Laminar boundary layer separation and reattachment on ablating and nonablating axisymmetric bodies at low Reynolds number and high Mach number
REATTACHED FLOW↗
Heat transfer and ablation rate measurement in Saturn S-II ullage motor exhaust plume Final report
Heat transfer and ablation rate measurement in Saturn S-II ullage motor exhaust plume
ROCKET EXHAUST↗
A study of artificial meteors as ablators
Simulated meteor entry tests in high enthalpy plasma jet to determine meteor ablation and radiation characteristics
PLASMA JET↗
Effect of composition, density, and environment on the ablative performance of phenolic nylon
Composition, density, and environmental effects on ablative performance of phenol resin and nylon mixture
NYLON↗
Determination of kinetic parameters of six ablation polymers by thermogravimetric analysis
Thermogravimetric analysis of ablating polymers to determine kinetic parameters describing mass loss due to thermal degradation
THERMOGRAVIMETRY↗
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↗