Search

Image Details

View Article Bookmark & Share

Choose export citation format:

Export Citation
Large resolution
Hi-Resolution Export to PDF

Uranus Orbiter and Probe: Mission Challenges and Concept Updates Since the Origins, Worlds, and Life Decadal Survey

  • Authors: Amy A. Simon, Richard C. Anderson, Daniel T. Gallagher, Michael J. Amato, Donald H. Ellison, Jacob A. Englander, Carl Engelbrecht, Noble Hatten, Richard S. Saylor, Chloe B. Beddingfield, Richard J. Cartwright, Nancy L. Chabot, Ian J. Cohen, Kathleen Mandt, Tom A. Nordheim, Lynnae C. Quick

Amy A. Simon et al 2026 The Planetary Science Journal 7 .

  • Provider: AAS Journals

Caption: Figure 3.

Deliverable mass for example SEP trajectories. For flight times of 12–14 yr, sufficient mass can be inserted in Uranus orbit with repeatable launch windows; if less delivered mass is required, flight times can be reduced further. This example uses the Hall PPS500 thruster performance (Englander et al. 2026).

Other Images in This Article
Image in this article
Image in this article
Image in this article
Image in this article
Image in this article
Image in this article
Image in this article
Image in this article
Image in this article

Show More

Copyright and Terms & Conditions

Additional terms of reuse