Investigation of hybrid rocket motors

Société: University of Arkansas, Little Rock, AK, USA
Publié: Mar 2011

Hybrid rocket motors contain a solid, inert fuel element and an oxidant that is pumped into contact with the fuel. This configuration is distinct from a liquid rocket where both the fuel (hydrogen) and the oxidant (oxygen) are mixed or a solid rocket where the fuel and oxidant are combined in the propellant grain. The research group at the University of Arkansas at Little Rock investigates fundamental aspects of combustion in hybrid rocket motors, for example thrust oscillations, pressure, plume flicker and acoustical output.



  • Anglais: Investigation of hybrid rocket motors PDF, 119 KB
  • Allemand: Untersuchung von Hybridraketentriebwerken PDF, 120 KB
Informations de base

Faire avancer l'innovation. Toujours à la pointe de l'évolution technologique.

S’abonner à nos newsletters, gérer ses abonnements ou se désabonner. La newsletter mensuelle contenant toutes les informations liées à l’aéronautique et défense.

Enable form call

At this point, an input form from Click Dimensions is integrated. This enables us to process your newsletter subscription. The form is currently hidden due to your privacy settings for our website.

External input form

By activating the input form, you consent to personal data being transmitted to Click Dimensions within the EU, in the USA, Canada or Australia. More on this in our privacy policy.