1. Choice of propulsion for some missiles
Readers are invited to refer to paragraph 2 of the article
[BM 3 000]
regarding the design of a propulsion system. Several examples are provided for illustrative purposes on tactical missile defense systems to begin identifying how to choose the type of aerospace propulsion based on the mission and operational constraints. The parameters and equations outlined in the articles
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Choice of propulsion for some missiles
Bibliography
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(1) - ANDERSON (J.D.) Jr -
Introduction to Flight.
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Fourth Edition, Mc Graw Hill (2000).
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(2) -
Recherche et technologie dans le groupe Snecma, propulsion aéronautique.
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Revue Scientifique et Technique...
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