An analysis is presented for the cost of the mission as a function of the following variables: amount of redundancy in the spacecraft, amount of care taken in building the spacecraft (functional and environmental tests, screening of components, quality control, etc), and the number of flights necessary to accomplish the mission. Thermal analysis and mathematical models for the experimental components are presented. The results of computer structural and stress analyses for support and cylinders are discussed. Reliability, quality control, and control system simulation by computer are also considered.


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    Title :

    Mission definition study for Stanford relativity satellite. Volume 3: Appendices


    Publication date :

    1971-12-22


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :