Propulsion Superiority Analysis of U-turn Launch Mode for Satellite Rocket

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概要

• 論文の詳細を見る

• This paper is based on the concepts of lagrangian Reynolds transport equation (LRTE), momentum, and the generalized total kinetic power of a rocket. The wood rocket model is used as a vivid model to explain propulsive efficiency of a rocket. We prove that the novel U-turn launch mode can convert total kinetic power and gravitational potential energy into rocket propulsive power. Furthermore, we use the first stage rocket engine of the Saturn V as an example to simulate and analyze its propulsive efficiency computationally with Matlab software. In conclusion, this revolutionary launch mode has the potential to dramatically improve the propulsive efficiency of launch vehicles.

• 2008-05-04

著者

• YUAN Kuang-Lin

  National Chung-Hsing University

• LEE Hsing-Juin

  National Chung-Hsing University

• LIN Hsu

  National Chung-Hsing University

• Lee Hsing-juin

  Dep. Of Mechanical Engineering National Chung-hsing Univ.

関連論文

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