An analysis of the coupled chemically reacting boundary layer and charring ablator, part 1 Summary report
Analyses and finite difference procedure for predicting transient in-depth response of charring ablation materials
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Analyses and finite difference procedure for predicting transient in-depth response of charring ablation materials
Total normal emittance measurements of charred ablator surfaces, discussing gas cap radiation effect
Heterogeneous reactions of molecular oxygen with thin film of carbonaceous char at low pressures
Visible and near IR spectral reflectance and emittance at high temperature of ablation chars, carbon and graphite
Oxygen depletion effect in chemical reactions between pyrolysis gases and air stream on surface recession of charring ablators
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
Rocket engine evaluation of erosion and char as functions of fabric orientation for silica reinforced nozzle materials
Pressure fields and multidimensional gas flow in permeable char layers and effects on ablation
Modified one-dimensional reaction kinetics program to allow for charring in three material layers of rocket nozzle throat insert case
Computer program development for charring ablative materials, chemically reacting laminar boundary layers, and turbulent boundary layer initiation
Simulated charring ablator performance during reentry phase
Thermochemical data from simulated pyrolysis gas flow through ablating char layer
Charring phenolic nylon ablator material pyrolysis and surface recession for cyclic and constant combined convective and radiative heating
Oxygen depletion effect in chemical reactions between pyrolysis gases and air stream on surface recession of charring ablators
Technique for manufacture of graphite composites uses high-char-forming processable polyimide resin systems to produce the graphitic matrix. Only three cyclic steps are required to yield a 99.7 percent graphite product.
Thermophysical and chemical properties of charring ablative materials
Ground test facility simulation of performance of charring ablators during atmospheric entry