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

Saeedipour, Hamid Reza and Mohd Yusof, lIIyia (2004) Range Optimization Using Trajectory Shaping Analysis Of A Surface-Launched Rocket. In: Proceedings National Conference on Engineering and Technology (NACET)., 26-27 May2004, Universiti Malaya.

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Abstract

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.

Item Type: Conference or Workshop Item (Paper)
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL780-785.8 Rocket propulsion. Rockets
Divisions: Kampus Kejuruteraan (Engineering Campus) > Pusat Pengajian Kejuruteraan Aeroangkasa (School of Aerospace Engineering)
Depositing User: ARKM Al Rashid Automasi
Date Deposited: 05 May 2009 06:57
Last Modified: 13 Jul 2013 04:14
URI: http://eprints.usm.my/id/eprint/9744

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