Altitude Maximization for Small Subsonic Low-Power Unguided Rockets

What is it about?

An unusual aspect of low-power rocketry is presented by describing a model of a launcher device with exhaust gases recovery capable of improving altitude performance. A wide number of different technical choices and possibilities have been analyzed. Although the study case refers to rockets of limited mass used in competition, the application of the model and the results obtained can be profitably considered even for larger rockets.

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