Hybridiraketti käyttää kahdessa eri olomuodossa olevaa ajoaineen komponenttia. Tavallisimmin polttoaine on kiinteä ja hapetin nestemäinen. Hapetin voisi periaatteessa olla kaasumainen.
Aiheesta muualla ROCKET PROPELLANTS Société regroupant des chercheurs de Stanford autour de développements sur la propulsion hybride Preliminary Analysis of Hybrid Rockets for Launching Nanosats into LEO Documents techniques de l'organisation anglaise Aspirespace Répertoire de liens vers des sites relatifs la propulsion hybride Aspirespace Introduction to hybrid design Developing and testing of a 2kN hybrid rocket engine Hybrid Rocket Engines, AspireSpace, membership-based organisation (in UK) (particularly see technical papers) Portland State Aerospace Society paraffin hybrid links Hybridrocket, Private page Design Optimization of Ground and Air-Launched Hybrid Rockets H2O2/Paraffin Hybrid Rockets for Launching Nanosats into LEO WARR, students developing hybrid engines University of Padua spin-off
Luokka:Raketit