An aerobraking orbital transfer vehicle (AOTV) (80) has aerobrake (82) with a blunted raked-off circular-cone configuration. The other components of the AOTV, including command/control module (95), fuel tanks (86, 88, 89 and 91), rocket engines (94) and afterbody (84), are positioned substantially along resultant force axis (104) of the AOTV (80). The axis (104) coincides with the resultant (sum of lift and drag) force vector. Afterbody (84) is mounted behind the aerobrake (82) with its length extending rearwardly from the aerobrake. The base flow clearance angle .phi. of the aerobrake (80) is 25.degree., thus allowing the afterbody (84) to extend rearwardly from the aerobrake (82) to a much greater extent than possible with a raked-off elliptic-cone aerobraking shield configuration. Afterbody size limitation and other problems associated with the raked-off elliptic-cone aerobraking shield configuration are alleviated by the combination of the aerobrake shape and positioning of the fuel tanks (86, 88, 89 and 91), rocket engines (94) and afterbody (84).


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    Titel :

    Raked circular-cone aerobraking orbital transfer vehicle


    Beteiligte:
    Park, Chul (Autor:in) / Davies, Carol B. (Autor:in)

    Erscheinungsdatum :

    27.02.1990


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aerobraking orbital transfer vehicle

    Scott, Carl D. / Nagy, Kornel / Roberts, Barney B. et al. | NTRS | 1989


    Aerobraking Orbital Transfer Vehicle

    C. D. Scott / K. Nagy / B. B. Roberts et al. | NTIS | 1985



    Design Study of an Integrated Aerobraking Orbital Transfer Vehicle

    C. D. Scott / B. B. Roberts / K. Nagy et al. | NTIS | 1985


    Raked stems

    Engineering Index Backfile | 1921