This paper presents data from the thermostructural testing of tape-wrapped carbon phenolic. This work has been performed with the use of a plasma torch and loading device in an effort to study the anomalous erosion characteristicfs of that seen in the Space Shuttle Solid Rocket Motor Nozzle STS-8A. Testing is conducted in an effort to determine conditions or parameters involved in this mode of failure.
Plasma torch testing for thermostructural evaluation of rocket motor nozzle materials
1989-07-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Solid rocket nozzle thermostructural behavior
AIAA | 1975
|Integrity and testing concerns of thermostructural materials
British Library Conference Proceedings | 1992
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