Method of predicting initial weight characteristics of Earth-launched single or multistage vehicle is proposed; approach to problem has been influenced by need for simplicity and directness, and attempt is made to coordinate both practical and theoretical aspects of stage weight allocation; basic considerations are outlined; to illustrate ease with which proposed method provides reasonable initial weight breakdown for vehicle, example is included.


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    Titel :

    Method of weight prediction of satellite launching vehicles


    Weitere Titelangaben:

    Spaceflight


    Beteiligte:
    Ball, K.J. (Autor:in) / Heyes, C.T. (Autor:in)

    Erschienen in:

    Spaceflight ; 9 , n 7


    Erscheinungsdatum :

    1967


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Optimization of staging and trajectory for satellite launching vehicles

    Matsubara, H. / Yamada, Y. / Nakanishi, H. | Engineering Index Backfile | 1966


    Optimization of staging and trajectory for satellite launching vehicles

    Matsubara, Hideo / Yamada, Yuji / Nakanishi, Hideki | TIBKAT | 1966



    MSAT satellite launching

    Online Contents | 1995


    Satellite launching possibilities

    Lyons, D.J. | Engineering Index Backfile | 1961