The evolution of capabilities and the current performance levels of the Delta launch vehicle are outlined. The first payload was the Echo I passive communications satellite, weighing 179 lb, and placed in GEO in 1960. Emphasis since then has been to use off-the-shelf hardware where feasible. The latest version in the 3924 first stage, 3920 second stage, and Pam D apogee kick motor third stage. The Delta is presently equipped to place 2800 lb in GEO, as was proven with the 2717 lb Anik-D1 satellite. The GEO payload placement performance matches the Shuttle's, and work is therefore under way to enhance the Delta performance to handle more massive payloads. Installation of the Castor-IV solid motor separation system, thereby saving mass by utilizing compressed nitrogen, rather than mechanical thrusters to remove the strap-on boosters, is indicated, together with use of a higher performance propellant and a wider nose fairing.


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    Titel :

    Delta capability for launch of communications satellites


    Beteiligte:
    Grimes, D. W. (Autor:in) / Russell, W. A., Jr. (Autor:in) / Kraft, J. D. (Autor:in)

    Erscheinungsdatum :

    1982-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Delta launch vehicle - Accommodations for small satellites

    Knox, K.-R. / Centre National d'Etudes Spatiales / European Space Agency | British Library Conference Proceedings | 1993