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Range Optimization Using Trajectory Shaping Analysis Of A Surface-Launched Rocket.

机译：使用弹道导弹的弹道成形分析进行射程优化。

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This paper is outlined the design and flight performance ot an advanced Surface-Launched Rocket. Brief descriptions of the technologies in the rocket design, parameters driving the rocket design & performance, the rocket performance prediction and examples of maximizing flight performance are presented.

机译：本文概述了高级水面发射火箭的设计和飞行性能。简要介绍了火箭设计中的技术，驱动火箭设计和性能的参数，火箭性能预测以及最大化飞行性能的示例。

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Saeedipour Hamid Reza; Mohd Yusof lIIyia;
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年度 2004
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原文格式 PDF
正文语种 {"code":"en","name":"English","id":9}
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入库时间 2022-08-31 14:51:45

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5. Object shape dependent kinematic manipulability measures for shape optimization, path planning, trajectory synthesis and part assembly [D] . Zhang, Shengzhong. 1997

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7. Range Optimization Using Trajectory Shaping Analysis Of A Surface-Launched Rocket. [O] . Saeedipour Hamid Reza, Mohd Yusof lIIyia 2004

机译：使用弹道导弹的弹道成形分析进行射程优化。
8. DESPOT. A Computer Scheme Optimizing the Propulsion Design and/or Trajectory of a Solid Propellant Rocket. [R] . feldman,lawrence a. 1977

机译：暴君。一种优化固体推进剂火箭推进器设计和/或轨迹的计算机方案。

Range Optimization Using Trajectory Shaping Analysis Of A Surface-Launched Rocket.

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