Ablative response of a silica phenolic to simulated liquid propellant rocket engine operating conditions
Ablative response of silica phenolic to simulated liquid propellant rocket engine operating conditions
Wool, M. R.↗
Engineering topics
Rindal, R. A.
Publications and source records attributed to Rindal, R. A..
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
Bartlett, E. P.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 2 - Finite difference solution for the in-depth response of charring materials considering surface chemical and energy balances
Computer program for finite difference equation analysis of in-depth response of materials exposed to high temperature environment
Moyer, C. B.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 4 - A unified approximation for mixture transport properties for multicomponent boundary-layer applications
Bifurcation approximation for binary and thermal diffusion coefficients, mixture viscosity, and thermal conductivity of laminar boundary layer
Bartlett, E. P.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 6 - An approach for characterizing charring ablator response with in-depth coking reactions
Coking reactions of pyrolysis gas in charring ablation material
Rindal, R. A.↗
Thermochemical ablation of rocket nozzle insert materials Final report
Resistance of rocket nozzle throat insert materials to corrosion and melting
Clark, K. J.↗
Experimental and theoretical analysis of ablative material response in a liquid- propellant rocket engine Final report
Ablative material degradation in liquid propellant rocket engine environment of nitrogen tetroxide-aerozine
Clark, K. J.↗
A multicomponent boundary layer chemically coupled to an ablating surface.
Incident of severe low level turbulence in clear air
CLEAR AIR TURBULENCE↗
Analytical and experimental study of ablation material for rocket engine application Final report
Techniques for rating performance of ablative materials in liquid-propellant rocket engines
ABLATING MATERIAL↗
Thermochemical ablation.
Thermochemical interaction between ablation material and environment during manned reentry, using mainly graphite and composite materials
REENTRY EFFECT↗
Analytical Evaluation of Rocket Nozzle Ablation
Method for calculating rates of material ablation in rocket nozzles
ROCKET NOZZLE↗