Publications related to the GRACE Missions (no abstracts)

Sorted by DateSorted by Last Name of First Author

Short–Period Mass Variations and the Next Generation Gravity Mission

Bender, P. L., Conklin, J. W., and Wiese, D. N., 2025. Short–Period Mass Variations and the Next Generation Gravity Mission. Journal of Geophysical Research (Solid Earth), 130(1):2024JB030290, doi:10.1029/2024JB030290.

Downloads

from the NASA Astrophysics Data System  • by the DOI System  •

BibTeX

@ARTICLE{2025JGRB..13030290B,
       author = {{Bender}, P.~L. and {Conklin}, J.~W. and {Wiese}, D.~N.},
        title = "{Short-Period Mass Variations and the Next Generation Gravity Mission}",
      journal = {Journal of Geophysical Research (Solid Earth)},
     keywords = {GRACE, gravity, mass change, accelerometer, gravitational reference sensor},
         year = 2025,
        month = jan,
       volume = {130},
       number = {1},
        pages = {2024JB030290},
     abstract = "{At the time that the 2017{\textendash}2027 Decadal Survey for Earth
        Science and Applications from Space was released, there was a
        strong emphasis on reducing the possibility of a substantial gap
        between the GRACE Follow-On mission and a successor mission.
        This has led to the subsequent rapid development of a successor
        mission in partnership between NASA and DLR, GRACE-Continuity
        (GRACE-C), expected to launch in 2028, to continue the
        timeseries of Earth system mass change established by GRACE and
        GRACE-FO. In parallel, ESA continues development of a pair of
        satellites called Next Generation Gravity Mission (NGGM),
        targeted for an inclination between 65{\textdegree} and
        75{\textdegree} to complement GRACE-C, launching in the early
        2030s. NGGM offers the possibility for reduced noise in
        measuring short-period variations in the satellite separation
        using an improved accelerometer relative to what is flying on
        GRACE-C. One pathway for this is by using a simplified version
        of the Gravitational Reference Sensors demonstrated on the LISA
        Pathfinder Mission in 2016. And, if the measurement accuracy is
        much improved, it appears desirable to fly NGGM with a fixed
        ground track and an approximately 5-day orbit repeat period.}",
          doi = {10.1029/2024JB030290},
       adsurl = {https://ui.adsabs.harvard.edu/abs/2025JGRB..13030290B},
      adsnote = {Provided by the SAO/NASA Astrophysics Data System}
}

Generated by bib2html_grace.pl (written by Patrick Riley modified for this page by Volker Klemann) on Mon Feb 16, 2026 23:51:55

GRACE-FO

Mon Feb 16, F. Flechtner