Add to ORKGThe shuttle orbiter relies primarily on a reusable surface insulation (RSI) thermal protection syste...
Investigation of low density ablative materials for heat shields on reentry vehicle
The packaging of metal wool for reusable thermal heat shields applied to aerodynamic and other surfa...
A material and process study was performed using subscale panels in an attempt to reduce the cost of...
The fabrication, testing, and evaluation of materials and techniques employed in the fabrication of ...
The major objectives were accomplished in three tasks: (1) modification of the ablative material com...
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 ...
The Apollo program to land men on the moon is administered by the National Aeronautics and Space Adm...
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...
The ablation performance of materials composed of various concentrations of nylon, hollow silica sph...
The Thermal Protection System (TPS) protects (insulates) a body from the severe heating encountered ...
The characteristics and development of a lightweight reusable thermal protection system for the spac...
A three-phase program to develop and demonstrate the feasibility of a metallic heat shield suitable ...
The shuttle orbiter relies primarily on a reusable surface insulation (RSI) thermal protection syste...
Investigation of low density ablative materials for heat shields on reentry vehicle
The packaging of metal wool for reusable thermal heat shields applied to aerodynamic and other surfa...
A material and process study was performed using subscale panels in an attempt to reduce the cost of...
The fabrication, testing, and evaluation of materials and techniques employed in the fabrication of ...
The major objectives were accomplished in three tasks: (1) modification of the ablative material com...
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 ...
The Apollo program to land men on the moon is administered by the National Aeronautics and Space Adm...
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...
The ablation performance of materials composed of various concentrations of nylon, hollow silica sph...
The Thermal Protection System (TPS) protects (insulates) a body from the severe heating encountered ...
The characteristics and development of a lightweight reusable thermal protection system for the spac...
A three-phase program to develop and demonstrate the feasibility of a metallic heat shield suitable ...
The shuttle orbiter relies primarily on a reusable surface insulation (RSI) thermal protection syste...
Investigation of low density ablative materials for heat shields on reentry vehicle
The packaging of metal wool for reusable thermal heat shields applied to aerodynamic and other surfa...