A separated nose section of a launch vehicle with an emergency rescue system (ERS) is a flight vehicle (FV) with a jet engine (JE) in the front position and with honeycomb lattice fins (LF) in the base region. The flight vehicle configuration is illustrated in Fig. I above the X-axis and a schematic of its scaled aerodynamic model is shown below the X-axis. Determination of aerodynamic characteristics (AC) for that sort of fight vehicle is a complicated problem which may be solved combining experimental techniques and theoretical calculations. Such work includes the following stages.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic Simulation and a Test Technique for Investigation of a Flight Vehicle with Jet Engine in Front Position and Lattice Fins


    Contributors:

    Publication date :

    2002


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Launch vehicle aerodynamic flight test results

    Gaines, L. M. / Osborn, W. L. / Wiltse, P. D. | NTRS | 1983



    Aerodynamic Test and Analysis of Wrap Around Fins with Base Cavities

    Abate, G. / Hathaway, W. / AIAA | British Library Conference Proceedings | 1994


    Aerodynamic Test and Analysis of Wrap Around Fins with Base Cavities

    Abate, G. / Hathaway, W. / AIAA | British Library Conference Proceedings | 1994


    Aerodynamic Prediction Methodology for Grid Fins

    Kretzschmar, R. W. / Burkhalter, J. E. / Research and Technology Organization et al. | British Library Conference Proceedings | 1998