AN ANALYTICAL INVESTIGATION OF ABLATION
Ablation relationships for any type of boundary layer from transpiration cooling results
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Ablation relationships for any type of boundary layer from transpiration cooling results
Ames atmosphere entry simulator and its use in determining characteristics of ethyl cellulose as ablative heat shield for ballistic missiles
Investigation in atmosphere entry simulator of nylon as ablative material for ballistic missiles
Effect of enthalpy variation on ablating materials
Spheres of ablating material subjected to aerodynamic heating to determine physical property
Ability of several ablating materials to reduce surface heat transfer in electric arc heated airstream
Ablation material for heat resistance against high thermal flux
Spacecraft reentry flight tests for determining performance of heat shields made of charring ablating material
Ablation of charring material by high velocity heated gas of different compositions - chemical reactions
Thermal radiation from ablating plastic materials injected into hypersonic shock waves
Ablation-type thermal protection of objects traversing an atmosphere - earth and mars
Reports on the ablation of teflon and polyethylene heat shields for low-angle reentry
Chemical interaction between an ablation system, a charring material and high-velocity streams of arc-heated air, nitrogen, and argon
Free flight investigations with solid fuel rocket propelled vehicle systems where the thermal protection was provided by either a subliming ablator or by transpiration cooling
Method for calculating rates of material ablation in rocket nozzles
Photometry, dimensions, and ablation rate of comets
Ablation behavior of charring material in high velocity streams of arc heated air, nitrogen, and argon
Approximate analysis of performance of charring ablators