The preliminary design of an earth-viewing spacelab payload, with accommodations shared by both NASA and ESA is addressed. Mission parameters for this flight include a launch date of September 1981, an inclination of 57 deg, and an orbital altitude of 325 km. A seven-day mission is planned. The NASA portion of this payload is assigned to the EVAL (Earth Viewing Applications Laboratory) program. The ESA complement is designed as a multiuser payload.


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    Title :

    EVAL System Concept Definition. Partial Spacelab Payload


    Publication date :

    1976


    Size :

    95 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English