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Improved Two-Impulse Transfer to Halo Orbits in Earth-Moon Elliptic Restricted Three Body Problem Framework Using Differential Evolution
By: Rithwik. N and R. V. Ramanan.
Pub. 2021, 20pgs.
PDF File. AAS 20-607.
Price: $29.00
 

Reprinted from Astrodynamics 2020, Advances in the Astronautical Sciences, Vol 175

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