Hybrid PPT–ABEP Propulsion for Extended CubeSat Missions in Very Low Earth Orbit
Abstract
All validation results and representative mission solutions presented in thissection are generated directly from the numerical framework described in thiswork, whose implementation is provided in the Code Availability section.
Fields of Study & Subjects
Spacecraft Dynamics and Control
Spacecraft Design and Technology
Space Satellite Systems and Control
Publication details
- Journal / source
- Zenodo (CERN European Organization for Nuclear Research)
- Publication date
- 17 January 2026