Nondimensional parameters are developed and plotted for use in rapid analysis of soft-landing system concepts for space vehicles; systems which automatically control and reduce vehicle energy remaining after main-stage retro-thrust, to zero at landing surface; mechanizations of some systems are presented and compared with optimum system in terms of energy consumption and ability to tolerate wide ranges of initial vehicle velocities and positions. (See also abstract in SAE -- J v 69 n 4 Apr 1961 p 92-6)


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    Titel :

    Mechanization of minimum-energy automatic lunar soft-landing systems


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Mears, C.M. (Autor:in) / Peterson, R.L. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Landing



    Erscheinungsdatum :

    1961


    Format / Umfang :

    110 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Mechanization of minimum-energy automatic lunar soft-landing systems

    Mears, C.M. / Peterson, R.L. | Engineering Index Backfile | 1961


    Mechanization of Minimum-Energy Automatic Lunar Soft-Landing Systems

    Mears, C. M. / Peterson, R. L. | SAE Technical Papers | 1963


    Automatic Landing Systems Mechanization - Series or Parallel Servos?

    Hoffman, Dale P. / Kawana, Harry | SAE Technical Papers | 1965