Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Messenger's Maneuvers to Reduce Orbital Period During the Extended Mission: Ensuring Maximum Use of the Bi-Propellant Propulsion System (AAS 13-382)



    Conference:

    23rd, Spaceflight mechanics meeting ; 2013 ; Kauai, HI



    Publication date :

    2013-01-01


    Size :

    14 pages


    Remarks:

    "Proceedings of the 23rd AAS/AIAA Space Flight Mechanics Meeting held February 10-14, 2013, Kauai, Hawaii."--Title page. Includes bibliographical references and indexes.




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    The First Three Maneuvers During Messenger's Low-Altitude Science Campaign (AAS 15-137)

    Flanigan, Sarah H. / Kirk, Madeline N. / O Shaughnessy, Daniel J. et al. | British Library Conference Proceedings | 2015


    Applying Experience from Mercury Encounters to MESSENGER's Mercury Orbital Mission (AAS 11-549)

    Page, B.R. / Williams, K.E. / Taylor, A.H. et al. | British Library Conference Proceedings | 2012


    Ensuring Cassini's end-of-mission propellant margins

    Sturm, Erick J. / Barber, Todd J. / Roth, Duane | IEEE | 2015


    Orbit Design and Navigation Through the End of Messenger's Extended Mission at Mercury (AAS 14-369)

    McAdams, J.V. / Bryan, C.G. / Moessner, D.P. et al. | British Library Conference Proceedings | 2014


    Ensuring Cassini's End-of-Mission Propellant Margins

    Sturm, Erick J., II / Barber, Todd J. / Roth, Duane | NTRS | 2015