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Orbits and Propagators - AGI

Orbits and Propagators - AGI

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Diseño de Vehículos Espaciales 1DVE1‐T07‐42Two‐impulse maneuvers: Hohmannv Initial velocity (r 1 )vv12rr1r2Final velocity (r 2 ) r1r r2a r rr re 2 r r2 rrr r r 2vrr 3 T arv1v v12r2r r r r1 21 1v2v2 vr22rr r 2r211

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