The article is devoted to the analysis of the trajectory parameters obtained during the flight experiment at the start of meteo-rocket MMP-06, to determine major parameters of motion of a round parachute at subsonic speeds in the range of altitudes from 0 to 60 km. The Reynolds number is changed in the range from 104 to1,5·106.The main parameters of the trajectory were obtained according to the experimental data. Only laboratory research on a model parachute systems in such a wide range of Reynolds numbers are found in the literature on parachute subjects. This article obtained results of flight experiment.


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    Title :

    PROCESSING AND ANALYSIS OF DATA OF natural experiment FOR DETERMINING THE tragectory CHARACTERISTICS OF A ROUND PARACHUTE AT HIGH ALTITUDES


    Contributors:
    S. V. Zhurin (author) / Yu. N. Gvozdev (author) / A. D. Lykov (author)


    Publication date :

    2016



    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown






    Parachute testing at altitudes between 30 and 90 kilometers.

    MCFALL, J.C. / MURROW, H. N. | AIAA | 1967


    PARACHUTE TESTING AT ALTITUDES BETWEEN 30 AND 90 KILOMETERS

    MCFALL, JR., JOHN / MURROW, HAROLD | AIAA | 1966


    Parachute Testing at Altitudes Between 30 and 90 Kilometers

    Gapcynski, J. P. / Mcfall, John C., Jr. / Murrow, Harold N. | NTRS | 1966