The major objectives were accomplished in three tasks: (1) modification of the ablative material composition for ease of fabrication as well as thermal and mechanical performance; (2) scaled-up, simplified, manufacturing techniques which resulted in cost reductions; and (3) the identification of a significant design problem caused by the differential pressure buildup imposed on mechanically attached ablative heat shield panels during launch
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Resistance to heat penetration and deformations or buckling of three ablation materials during simul...
Investigation of low density ablative materials for heat shields on reentry vehicle
The fabrication, testing, and evaluation of materials and techniques employed in the fabrication of ...
A material and process study was performed using subscale panels in an attempt to reduce the cost of...
Fabrication of prototype low density ablative heat shield panels for space shuttles with production ...
Ablator heat shield configuration optimization studies were conducted for the orbiter. Ablator and r...
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
A heat shield for a space vehicle comprises a plurality of phenolic impregnated carbon ablator (PICA...
Ablating materials tested at combined radiative and convective heating for manned reentry vehicle he...
Refurbishable composite thermostructural heat shield panels for manned lifting entry vehicle
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
A three-phase program to develop and demonstrate the feasibility of a metallic heat shield suitable ...
The Apollo program to land men on the moon is administered by the National Aeronautics and Space Adm...
The effects of heat load, ablator density, and backup structure, etc. upon the heat shield performan...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Resistance to heat penetration and deformations or buckling of three ablation materials during simul...
Investigation of low density ablative materials for heat shields on reentry vehicle
The fabrication, testing, and evaluation of materials and techniques employed in the fabrication of ...
A material and process study was performed using subscale panels in an attempt to reduce the cost of...
Fabrication of prototype low density ablative heat shield panels for space shuttles with production ...
Ablator heat shield configuration optimization studies were conducted for the orbiter. Ablator and r...
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
A heat shield for a space vehicle comprises a plurality of phenolic impregnated carbon ablator (PICA...
Ablating materials tested at combined radiative and convective heating for manned reentry vehicle he...
Refurbishable composite thermostructural heat shield panels for manned lifting entry vehicle
Results are presented from an investigation to determine the effects of fabrication-induced defects ...
A three-phase program to develop and demonstrate the feasibility of a metallic heat shield suitable ...
The Apollo program to land men on the moon is administered by the National Aeronautics and Space Adm...
The effects of heat load, ablator density, and backup structure, etc. upon the heat shield performan...
Ablation behavior of heat shield of Apollo command module over wide range of thermal environment
Resistance to heat penetration and deformations or buckling of three ablation materials during simul...
Investigation of low density ablative materials for heat shields on reentry vehicle