Topics

No keywords indexed for this article. Browse by subject →

References
23
[3]
Golan O. M. (1990)
[5]
Three-stage approach to optimal low-thrust Earth-moon trajectories

Bion L. Pierson, Craig A. Kluever

Journal of Guidance, Control, and Dynamics 10.2514/3.21344
[6]
Kluever C. A. Journal of the Astronautical Sciences (1994)
[9]
Aston G. Aerospace America (1987)
[15]
15Szebehely, V. G., Theory of Orbits, the Restricted Problem of Three Bodies, Academic, New York, 1967, pp.7-21.
[16]
Egorov V. A. (1969)
[17]
Anon (1989)
[19]
Pierson B. L. (1988)
[20]
Bryson A. E. (1975)
[23]
Dixon L. C. W. Aeronautical Journal (1972) 10.1017/s0001924000042731
Cited By
27
Indirect Optimization of Spiral Trajectories

Christopher L. Ranieri, Cesar A. Ocampo · 2006

Journal of Guidance, Control, and D...
Metrics
27
Citations
23
References
Details
Published
Mar 01, 1997
Vol/Issue
20(2)
Pages
239-245
Cite This Article
Craig A. Kluever, Bion L. Pierson (1997). Optimal Earth-Moon Trajectories Using Nuclear Electric Propulsion. Journal of Guidance, Control, and Dynamics, 20(2), 239-245. https://doi.org/10.2514/2.4058
Related

You May Also Like