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- W2036989595 abstract "If the flow of booster gas which is exhausted to the rear part of a canister is properly restricted in the canister of a hot-launch system, the resultant pressure built up in the canister provides additional force to accelerate the missile to a required launch velocity. These thrust augmentation performances can be controlled through the configuration design of baseplate orifices. In this paper, the simple technique to analyze the thrust augmentation performances of baseplate orifices is suggested and the thrust augmentation characteristics by its various configurations are compared. According to the initial displacement of a missile, the inner pressure of a canister is measured from scaled cold flow tests, and the discharge coefficient of baseplate orifices is calculated. Then the thrust augmentation in a canister is simulated by applying these discharge characteristics to the AMESIM software for launch dynamics." @default.
- W2036989595 created "2016-06-24" @default.
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- W2036989595 date "2011-12-05" @default.
- W2036989595 modified "2023-09-24" @default.
- W2036989595 title "Analysis of the Thrust Augmentation in the Canister with Baseplate Orifices" @default.
- W2036989595 cites W112623685 @default.
- W2036989595 cites W2056112432 @default.
- W2036989595 doi "https://doi.org/10.9766/kimst.2011.14.6.1067" @default.
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