Mathematical model and technical solution for small multistage suborbital launchers

The paper purpose is to dignify some aspects regarding the calculus model and technical solutions for small multistage suborbital launchers used to test spatial equipment and scientific measurements. The calculus methodology consists in numerical simulation of launcher evolution for different start...

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Bibliographische Detailangaben

Hauptverfasser:	Chelaru, T.-V., Barbu, C., Chelaru, A.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamics Calculus Earth Electronic mail Engines launcher Mathematical model multistage Performance analysis Recycling Rockets simulation suborbital Testing
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