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航空宇宙システムarXiv:2104.11831

ドローン発射短距離ロケットの概念

Drone Launched Short Range Rockets

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ドローンや航空機から高高度・高速で放出し、低燃焼速度モーターで上昇後に弾頭を放出して長距離を高速度で攻撃するDLSRRの概念を理論解析とMATLAB計算で示した論文。

著者: Mikhail Shubov

分類: cs.RO

原文アブストラクト

A concept of drone launched short range rockets (DLSRR) is presented. A drone or an aircraft rises DLSRR to a release altitude of up to 20 $km$. At the release altitude, the drone or an aircraft is moving at a velocity of up to 700 $m/s$ and a steep angle of up to 68$^o$ to the horizontal. After DLSRRs are released, their motors start firing. DLSRRs use slow burning motors to gain altitude and velocity. At the apogee of their flight DLSRRs release projectiles which fly to the target and strike it at high impact velocity. The projectiles reach a target at ranges of up to 442 $km$ and impact velocities up to 1.88 $km/s$. We show that a rocket launched at high altitude and high initial velocity does not need expensive thermal protection to survive ascent. Delivery of munitions to target by DLSRRs should be much less expensive than delivery by a conventional rocket. %% Even though delivery of munitions by bomber aircraft is even less expensive, a bomber needs to fly close to the target, while a DLSRR carrier releases the rockets from a distance of at least 200 $km$ from the target. %% All parameters of DLSRRs, and their trajectories are calculated based on theoretical (mechanical and thermodynamical) analysis and on several MatLab programs.

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