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Posted by David Williams on November 8, 2005, 10:05 am
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-> Can any one suggest me an efficient orbit to fly a space craft from the
-> L1 lagrange point to mars sun-synchronous orbit? Thank you
It's just a Hohmann transfer orbit, with its perihelion at the distance
of the L1 point and its aphelion at the distance of Mars. I posted the
calculations for an orbit from Earth to Mars here a few months ago. The
changes to use the L1 point would be minor.
dow
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