The ablation performance of materials composed of various concentrations of nylon, hollow silica spheres, hollow phenolic spheres, and four elastomeric resins was determined. Both blunt-body and flat-panel specimens were used, the cold-wall heating-rate ranges being 0.11 to 0.8 MW/sq m, respectively. The corresponding surface pressure ranges for these tests were 0.017 to 0.037 atmosphere and 0.004 to 0.005 atmosphere. Some of the results show that (1) the addition of nylon significantly improved the ablation performance, but the nylon was not compatible with one resin system; (2) panel and blunt-body specimen data do not show the same effect of phenolic sphere content on ablation effectiveness; and (3) there appears to be an optimum concent...
Ablatives are materials used to protect the inner hardware of aerospace structures from the inimical...
Fabrication of prototype low density ablative heat shield panels for space shuttles with production ...
Lightweight ceramic ablators (LCA's) were recently developed at Ames to investigate the use of low d...
Theoretical analysis of five composite ablation materials with various percentages of phenolic resin...
Thermophysical properties of nondegradated and thermally degradated low density phenolic-nylon ablat...
Thermal and mechanical properties data were obtained for a low density elastomeric resin based ablat...
Thermophysical property data for ablation materials - aerodynamic heating of low density phenolic ny...
Exploratory investigation of nylon grain size effect on ablation of phenolic nylo
Spherically blunted 0.44-radian (25 deg) half-angle conical models coated with elastomeric ablative ...
For thermal protection materials (TPMs) which are used to protect space vehicles from extreme thermo...
Influence of environmental conditions on thermal performance of low density charring ablato
Investigation of low density ablative materials for heat shields on reentry vehicle
Resistance to heat penetration and deformations or buckling of three ablation materials during simul...
An ablator patch material performed well in an arc plasma environment simulating nominal Earth entry...
Elastomeric and rigid silicone, epoxy, and phenol resin base ablating materials evaluated at various...
Ablatives are materials used to protect the inner hardware of aerospace structures from the inimical...
Fabrication of prototype low density ablative heat shield panels for space shuttles with production ...
Lightweight ceramic ablators (LCA's) were recently developed at Ames to investigate the use of low d...
Theoretical analysis of five composite ablation materials with various percentages of phenolic resin...
Thermophysical properties of nondegradated and thermally degradated low density phenolic-nylon ablat...
Thermal and mechanical properties data were obtained for a low density elastomeric resin based ablat...
Thermophysical property data for ablation materials - aerodynamic heating of low density phenolic ny...
Exploratory investigation of nylon grain size effect on ablation of phenolic nylo
Spherically blunted 0.44-radian (25 deg) half-angle conical models coated with elastomeric ablative ...
For thermal protection materials (TPMs) which are used to protect space vehicles from extreme thermo...
Influence of environmental conditions on thermal performance of low density charring ablato
Investigation of low density ablative materials for heat shields on reentry vehicle
Resistance to heat penetration and deformations or buckling of three ablation materials during simul...
An ablator patch material performed well in an arc plasma environment simulating nominal Earth entry...
Elastomeric and rigid silicone, epoxy, and phenol resin base ablating materials evaluated at various...
Ablatives are materials used to protect the inner hardware of aerospace structures from the inimical...
Fabrication of prototype low density ablative heat shield panels for space shuttles with production ...
Lightweight ceramic ablators (LCA's) were recently developed at Ames to investigate the use of low d...