For supersonic and hypersonic flight conditions with ramjets, trajectory calculations have to be coupled with the engine performances. In space transportation systems ramjet will be used in a relatively wide range of Mach numbers, and therefore not always near the optimum design point. Optimization of several physical parameters along the trajectory will be inevitable. Some of these parameters are discussed along with their importance for an ascent trajectory, having a minimum fuel requirement.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Ramjet Engines Performance

    Ingenito, Antonella | Springer Verlag | 2021


    Fundamentals of Ramjet Engines

    Ingenito, Antonella | Springer Verlag | 2021


    Ramjet engines for spacecraft

    Stechkin, B. | NTRS | 1967


    Critical considerations in the design of supersonic combustion ramjet /scramjet/ engines

    WALTRUP, P. J. / BILLIG, F. S. / EVANS, M. C. | AIAA | 1981


    Material Selection for Ramjet Engines

    Ingenito, Antonella | Springer Verlag | 2021