Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Trajectory optimization method in two-stage-to-orbit RBCC-RKT launch vehicle



    Published in:

    Publication date :

    2014



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Chinese



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik



    Trajectory Development and Optimization of an RBCC-Based Launch Vehicle (AAS 99-347)

    Hack, K. J. / Riehl, J. P. / American Astronautical Society et al. | British Library Conference Proceedings | 2000


    Design and Optimization of RBCC Powered Suborbital Reusable Launch Vehicle

    Gong, Chunlin / Chen, Bin / Gu, Liangxian | AIAA | 2014



    Application of a New Economic Analysis Tool to a Two-Stage-to-Orbit RBCC Launch Vehicle Design

    Olds, J. / Lee, H. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996


    Design and Optimization of RBCC Powered Suborbital Reusable Launch Vehicle (AIAA 2014-2361)

    Gong, C. / Chen, B. / Gu, L. et al. | British Library Conference Proceedings | 2014