Interest in the outer planets of our solar system remains high following several recent high profile missions. These science missions to the outer planets require significant energy to deliver payloads. This energy typically results in either multiple planetary flybys or very small payloads or both. NASA's Space Launch System (SLS) heavy launch vehicle is being developed as part of NASA's directive to return to the moon, followed by crewed missions to Mars. Along with delivering crew to cislunar space, SLS will also have the capability to launch science payloads for high energy outer planet missions. Adding a kick stage on top of SLS further increases SLS's capability for these missions. This paper discusses the capability of SLS, both alone and with kick stages, to deliver payloads for outer planet missions. There are currently a number of solid motors that could be used as kick stages, and this paper analyzes the results, advantages, and disadvantages of using these motors along with SLS to deliver larger payloads with shorter mission times for outer planet science missions.


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    Title :

    SLS with Kick Stages for Outer Planet Missions


    Contributors:


    Publication date :

    2019-03-01


    Size :

    4442203 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    SLS with Kick Stages for Outer Planet Science Missions

    Haws, Terry / Fuller, Michael | AIAA | 2018


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    Haws, Terry / Fuller, Michael | British Library Conference Proceedings | 2018