PDS4 CERTIFIED










    Polar view of Jupiter by Juno JUNOCAM at Perijove 72.
    Credit: NASA/JPL-Caltech/SwRI/MSSS/Kevin M. Gill © CC BY



    Description

    Juno is a spin-stabilized spacecraft, powered by 3 large, deployable rigid-panel arrays that can be moved to adjust the spin axis relative to the high gain antennae boresight. The spacecraft utilizes high energy density Li ion batteries for battery-regulated bus voltage. Basic radiation protection for sensitive electronics is afforded by a titanium-walled vault.  Telecom is achieved with X-band uplink and downlink. Ka-band telecom is included for improved Doppler measurement performance

    References

    Kim, B., Kwon, G., Kim, K., & Ye, J. C. 2024, in ICLR

    Punnappurath, A., Abuolaim, A., Abdelhamed, A., Levinshtein, A., & Brown, M. S. 2022, in Proceedings of the IEEE/CVF Conference on Computer Vision and Pattern Recognition (CVPR)

    Simon, A. A., Wong, M. H., & Orton, G. S. 2015, The Astrophysical Journal, 812, 55, https://doi.org/10.1088/0004-637X/812/1/55">doi: 10.1088/0004-637X/812/1/55

    Zhu, J.-Y., Park, T., Isola, P., & Efros, A. A. 2017, in Computer Vision (ICCV), 2017 IEEE International Conference on ??????????

    Accessing the Data

    The data has 2 components:

    Data calibrated, A series of tif files of images for individual orbits
    Data mosaics, A series of fits files

    The User’s guide
    Calibrated Index (csv)
    Mosaic Index (csv)


    Citations

    PDS recommendations for citing data sets can be found here.

    Georgakis, G., S. Ramanakumar, E.K. Dahl (2025). JunoCam - Machine Learning Calibration Bundle, NASA Planetary Data System, https://www.doi.org/10.17189/ryea-mj65.