Analytical study of longitudinal perturbations to steady orbital flight of lifting self-propelled vehicle in circular orbit; calculations are performed with linear and nonlinear equations for set of aerodynamic and inertial parameters, and altitudes from 100,000 to 700,000 ft; applicability to entry or glide phase and to sustained flight of self-propelled sub-satellite describing steady circular orbit.


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    Title :

    Longitudinal dynamics of lifting vehicle in orbital flight


    Additional title:

    J Aerospace Sciences


    Contributors:
    Etkin, B. (author)

    Published in:

    Publication date :

    1961


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Nonlinear longitudinal dynamics of an orbital lifting vehicle

    Dobrzelecki, A. J. / Vinh, N. X. | NTRS | 1971


    APPROXIMATE LONGITUDINAL DYNAMICS OF A LIFTING ORBITAL VEHICLE

    MEIER, T. C. / NORMAN, W. S. | AIAA | 1963


    Non-linear longitudinal dynamics of an orbital lifting vehicle

    Dobrzelecki, A. J. / Vinh, N. X. | NTRS | 1969


    Non-linear longitudinal dynamics of an orbital lifting vehicle.

    Dobrzelecki, A. J. / Vinh, N. X. | NTRS | 1969


    Non-Linear Longitudinal Dynamics of an Orbital Lifting Vehicle

    A. J. Dobrzelecki / N. X. Vinh | NTIS | 1969