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A Study on the Influence of Helicopter Main Rotor Inflow Model upon Launched Rocket Trajectory and Safe Launch Envelope
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헬리콥터 유입류 모델에 따른 발사된 로켓의 비행궤적 영향성 및 안전발사 기동영역 해석 연구

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Type
Academic journal
Author
Chang Deok Yang (한국항공우주산업) Dong Woo Jung (한국항공우주산업)
Journal
항공우주시스템공학회 Journal of Aerospace System Engineering Vol. 13 No. 3 KCI Accredited Journals
Published
2019.6
Pages
70 - 77 (8page)

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A Study on the Influence of Helicopter Main Rotor Inflow Model upon Launched Rocket Trajectory and Safe Launch Envelope
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This study presents the numerical investigation of the trajectory of rocket launched from a helicopter. The nonlinear mathematical model of armed configuration of UH-60 helicopter was developed while Hydra 70 unguided rocket was modeled to simulate the rocket behavior. The effects of various inflow models on the launched rocket trajectory are obtained. Similarly, rocket launch simulation was performed to determine the unsafe flight maneuver condition where the rocket trajectory is critically close to the helicopter main rotor tip path plane.

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