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- W2754364915 abstract "Ablation cooling in rocket engine with combustion chamber liner and nozzle constructed of silica phenolic ablative material" @default.
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- W2754364915 date "1971-08-01" @default.
- W2754364915 modified "2023-09-26" @default.
- W2754364915 title "Application of Ablation to a High Chamber Pressure Rocket Engine" @default.
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