Disseny del sistema d'ignició d'un motor de combustible sòlid

Le résumé fourni par la source

The study that has been developed in the following academic work deal with the design of an engine of solid propellant ignition system to collaborate with a project named WikiSat. Its main objective is to place a femto-satellite, whose mass is below 100 grams, in a LEO (Low earth Orbit) orbit. As detailed below, the two theoretical solutions presented have as an objective to produce the propellant ignition of the engine rocket at an altitude of 35 km, taking into account that the mass of the launcher cannot exceed 100 kg.

Ce résumé expose les affirmations des auteurs. BNTIC ne l’interprète pas comme une validation indépendante des résultats.