The Space Shuttle's unique design features include multiple re-uses of its major elements, large cargo carrying capacity, and the capability of deploying, servicing, and retrieving a variety of payloads. These design features, i.e., reusability and cargo flexibility, were incorporated to satisfy the objective of providing a transportation system which will lower the cost of delivering a variety of payloads to the earth orbit. The Space Shuttle System consists of a reusable manned Orbiter containing three main engines, two reusable Solid Rocket Boosters, and an expendable External Tank containing propellant for the Orbiter main engines. On a typical Space Shuttle mission, the Orbiter will remain in orbit for up to 7 days conducting on-orbit observations and operations, return to earth with personnel and payload, land horizontally on a runway, and be readied for another flight in as few as 14 days. Another mission class includes deploying, servicing, and recovering satellites.


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    Titel :

    Space Shuttle Program - An overview


    Beteiligte:
    Kloves, T. R. (Autor:in)

    Kongress:

    Communications Satellite Systems Conference ; 1976 ; Montreal, Canada


    Erscheinungsdatum :

    01.04.1976


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Space Shuttle Program overview.

    Everline, R. T. | NTRS | 1973


    Space Shuttle Program - An overview

    KLOVES, T. | AIAA | 1976


    Space Shuttle Program: An Overview

    Jarett, David | AIAA | 1977