Contained in the report are the results of systematic calculations of the NIRO vehicle performance capabilities. These capabilities were determined by computing the vehicle trajectory characteristics for various payload weights and configurations. Trajectory parameters are presented as time-histories of velocity, altitude, range, flight path angle, Mach Number, and dynamic pressure. From these data, summary curves are provided giving velocity and altitude at major time points (i.e., stage ignition, burnout, and apogee) as a function of payload weight, and plots showing apogee altitude and impact range as a function of payload weight and launch angle (with constant apogee time lines). A set of data are given for each payload configuration. Also, included for information, are the vehicle weight, propulsion, and drag data used in these computations. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerodynamic and Flight Performance Analysis for the Niro Sounding Rocket


    Contributors:
    J. P. Taylor (author) / A. M. Olson (author)

    Publication date :

    1966


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Kia Niro

    Allen,J. / Kia Motors,KR | Automotive engineering | 2016


    Flight analysis of sounding rocket

    Malina, F.J. / Smith, A.M.O. | Engineering Index Backfile | 1938


    THE DETERMINATION OF AERODYNAMIC STABILITY COEFFICIENTS FROM SOUNDING ROCKET FLIGHT DATA

    NICOLAIDES, JOHN / EIKENBERRY, ROBERT / INGRAM, CHARLES | AIAA | 1967