Charring ablation performance in turbulent flow. Volume 1 - Analytical and experimental studies
Semiempirical correlation techniques for predicting charring ablation performance of Apollo heat shield in turbulent flow
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Semiempirical correlation techniques for predicting charring ablation performance of Apollo heat shield in turbulent flow
FORTRAN 4 program for predicting charring ablation performance of Apollo heat shield in turbulent flow
Transmission loss and effects on antenna radiation patterns and impedance produced by thermally degraded ablation materials
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat shields
Comparative evaluation of ablative materials in arc plasma jets
Transient thermal analysis and structural analysis for synthesis of ablating thermostructural panels in planetary entry environment
Pressure fields and multidimensional gas flow in permeable char layers and effects on ablation
Computer program development for charring ablative materials, chemically reacting laminar boundary layers, and turbulent boundary layer initiation
Thermal and mechanical properties of phenolic nylon ablation materials
Ablative materials examination before and after test firing
Ablation product absorption and line transitions effects on shock layer radiative transport around blunt body
Investigation of low density ablative materials for heat shields on reentry vehicles
Simulated charring ablator performance during reentry phase
Ablation behavior of heat shield of Apollo command module over wide range of thermal environments
Ablative effectiveness of low density phenolic nylon materials
Design of injectors and ablative thrust chambers for FLOX propane rocket engine with 1.2 inch throat diameter
Throat and nozzle insert design for ablative rocket engine using storable propellants
Chemical equilibrium of ablation materials including condensed species