Hybrid propulsion and new launch systems  

Definition of propulsion by rocket : static performance of rockets for launch to space missions ; definition of thrust and drag ; equation of motion of a rocket ; state variables and control ; constraints on the trajectory . Performance of singlestage and multistage rocket . Definition of thrust requirements for performing space missions. Definition and classification of Propellants for hybrid engines. Process Combustion : subsonic combustion . Influence of the initial conditions of the propellant . Calculation of the temperature of combustion in conditions of chemical equilibrium. Sizing and design procedures for (a) Injection system (injectors), (b) nozzle, (c) thrust chamber. New launch systems: (a) gun launch to orbit ( ram accelerator and railgun ), (b) launch from aircraft in subsonic flight, (c) airbreathing SSTO launch vehicles.
Presential
English
Hybrid propulsion and new launch systems
English

Funded by the European Union. Views and opinions expressed are however those of the author(s) only and do not necessarily reflect those of the European Union or HaDEA. Neither the European Union nor the granting authority can be held responsible for them. The statements made herein do not necessarily have the consent or agreement of the ASTRAIOS Consortium. These represent the opinion and findings of the author(s).