Design of a Hybrid Chemical/Electric Propulsion Orbital Transfer Vehicle
Author:
Affiliation:
1. Purdue University, West Lafayette, Indiana 47907-1282
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3791
Reference25 articles.
1. Spacecraft Electric Propulsion-An Overview
2. Electric power system development - A companion technology to electric propulsion
3. Designing continuous-thrust low-Earth-orbit to geosynchronous-Earth-orbit transfers
4. Optimal Low-Earth-Orbit-Geostationary-Earth-Orbit Intermediate Acceleration Orbit Transfer
5. Optimization of very-low-thrust, many-revolution spacecraft trajectories
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