Design of Interplanetary Hybrid CubeSat and SmallSat Propulsion Systems
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4668
Reference18 articles.
1. MarCO: Interplanetary Mission Development On a CubeSat Scale
2. Cost effective propulsion systems for small satellites using butane propellant
3. CubeSat High-impulse Adaptable Modular Propulsion System (CHAMPS) Product Line Development Status and Mission Applications
4. Hybrid rocket propulsion systems for outer planet exploration missions
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