Conceptual Neptune orbiter was designed for the purpose of assessing mission feasibilityBuilt off of the 2017 Pre-Decadal Study, but adapted for drag modulation aerocapture.Science payload includes: Narrow Angle camera, Doppler Imager, Magnetometer, Atmospheric Probe (w/ ASI, Nephelometer, Mass Spectrometer). Baseline concept of operations releases probe prior to orbit insertion, but investigations are ongoing to assess the feasibility of bringing the probe to orbit before release.


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    Titel :

    A Neptune Orbiter Concept Using Drag Modulated Aerocaptue (DMA) and the Adaptable, Deployable Entry and Placement Technology (ADEPT)


    Beteiligte:
    Wercinski, P. (Autor:in) / Austin, A. (Autor:in) / Nelessen, A. (Autor:in) / Strauss, B. (Autor:in) / Hogstrom, K. (Autor:in) / Landau, D. (Autor:in) / Luthman, E. (Autor:in) / Ravich, J. (Autor:in) / Lobbia, M. (Autor:in) / Allen, G. (Autor:in)

    Kongress:

    Outer Planets Assessment Group Meeting ; 2019 ; Washington, DC, United States


    Erscheinungsdatum :

    2019-04-23


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :