2018
DOI: 10.1007/s42423-018-0020-6
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Thermo-structural Analysis of Solid Rocket Scarfed Nozzle with Composite Ablative Liners for Crew Escape Solid Motor

Abstract: Crew escape system (CES) is one of the most critical subsystems in a human-rated launch vehicle. CES has four different types of solid motors. One is the high-altitude escape motor (HEM). This motor has the scarfed nozzle region at the divergent aft-end side which is different from conventional nozzle to accommodate the nozzle inside the envelope of the crew module shroud. The composite ablative phenolic liners are bonded to the nozzle metallic hardware by means of adhesive. The structural integrity of this sc… Show more

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Cited by 1 publication
(1 citation statement)
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“…It can be widely used in adhesives and insulating materials [4][5][6]. And phenolic resin-based composite materials have the advantages of low cost, good heat resistance, flame retardancy, and corrosion resistance, which can be widely used as thermal protection materials in the aerospace field, especially used in key components such as the expansion section of rocket engine nozzle [7][8][9][10][11][12].…”
mentioning
confidence: 99%
“…It can be widely used in adhesives and insulating materials [4][5][6]. And phenolic resin-based composite materials have the advantages of low cost, good heat resistance, flame retardancy, and corrosion resistance, which can be widely used as thermal protection materials in the aerospace field, especially used in key components such as the expansion section of rocket engine nozzle [7][8][9][10][11][12].…”
mentioning
confidence: 99%