A correlation of sonic boom pressure signatures recorded during reentry of the Apollo 15 command module with wind-tunnel signatures extrapolated to flight distances has been made for Mach numbers of 1.16 and 4.57. The flight pressure signatures were recorded by pressure sensors located onboard ships positioned near the ground track while the wind-tunnel signatures were measured during tests of a 0.016-scale model of the command module. The agreement between estimates based on wind-tunnel data and flight measurements was better at Mach 4.57 than at Mach 1.16.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    A Wind Tunnel Flight Correlation of Apollo 15 Sonic Boom


    Contributors:

    Publication date :

    1972-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    A wind tunnel flight correlation of Apollo 16 sonic boom

    Garcia, F., Jr. / Hicks, R. M. / Mendoza, J. P. | NTRS | 1973


    A Wind Tunnel Flight Correlation of APOLLO 16 Sonic Boom

    F. Garcia / R. M. Hicks / J. P. Mendoza | NTIS | 1973


    A Wind Tunnel Flight Correlation of APOLLO 15 Sonic Boom

    R. M. Hicks / J. P. Mendoza / F. Garcia | NTIS | 1972



    Wind-Tunnel Sonic-Boom Testing Techniques

    Carlson, H. W. / Morris, O. A. | NTRS | 1966