Development of low cost ablative nozzles for solid propellant rocket motors, volume 1 Final report
Evaluating low cost ablative materials for use in large solid propellant rocket motors
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Evaluating low cost ablative materials for use in large solid propellant rocket motors
Performance tests for ablative materials subjected to high intensity carbon dioxide laser radiation
Resin systems for matrix material in ablative composite for liquid rocket combustion chambers using fluorine-containing propellants
Dual ablation measurement technique using nucleonic methods for tracing char and char virgin material interface recessions
Shock-wave shapes and surface pressures on hemisphere and cone cylinders in low density hypersonic flow including ablation
Determining composition of pyrolysis products from degradation of ablative materials
Summary of material and design improvements to reduce ablative chamber throat erosion in lunar module descent engine
Grove patterns on ablated surfaces of Teflon 8-foot high temperature structures tunnel
Effects of ablative discrepancies on nozzle performance reliability
Conservation equations for analysis of interaction of ablating protection systems and stagnation region heating
Injector compatibility improvement for Apollo lunar module descent engine ablative chamber
Evaluation of ablation heat shield material incorporating electrical connectors
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablator
Computer program for predicting charring ablation performance of heat shielding
Apollo ablator thermal performance at superorbital entry velocities
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic boundary layers
Char formation and surface recession of composite ablation material with silicone resin base
Coupled computer code for transient thermal response and ablation of noncharring heat shields and nose tips