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Introductory Physics Homework Help
Hohmann Transfer Orbit (Simple)
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[QUOTE="gneill, post: 4531400, member: 293536"] If I may suggest, perhaps an easier to use formula for the velocity of a body on orbit is given by: $$v(r) = \sqrt{\mu \left(\frac{2}{r} - \frac{1}{a} \right)}$$ where ##\mu## is the gravitational parameter of the central body (GM for the Earth in this case). You know the perigee radius and a for the transfer orbit... so no mucking about with AU and periods. [/QUOTE]
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Introductory Physics Homework Help
Hohmann Transfer Orbit (Simple)
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