Computation of optimal Mars trajectories via combined chemical/electrical propulsion, Part 3: Compromise solutions

Author:

Miele A.,Wang T.,Williams P.N.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. A. Miele, T. Wang, P.N. Williams, Computation of optimal Mars trajectories via combined chemical/electrical propulsion, Part 1, Paper IAC-02-A.6.05, 53rd International Astronautical Congress, Houston, Texas, 2002.

2. A. Miele, T. Wang, P.N. Williams, Computation of optimal Mars trajectories via combined chemical/electrical propulsion, Part 2: Minimum time solutions with bounded thrust direction, Paper AAS-03-121, 13th Annual AAS/AIAA Space Flight Mechanics Meeting, Ponce, Puerto Rico, 2003.

3. How shall we go to Mars? A review of mission scenarios;Walberg;Journal of Spacecraft and Rockets,1993

4. Mars sample return project;O’Neil;Acta Astronautica,2000

5. Optimal transfers from an Earth orbit to a Mars orbit;Miele;Acta Astronautica,1999

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1. Minimum fuel trajectories for round trip lunar missions;Computational and Applied Mathematics;2017-11-17

2. Optimal round trip lunar missions based on the patched-conic approximation;Computational and Applied Mathematics;2015-06-07

3. Optimal Mars transfers for small payload transportation;Celestial Mechanics and Dynamical Astronomy;2009-12-30

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