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Discussion :: GATE Aeronautical Engineering

  1. The Hohmann ellipse used as earth-Mars transfer orbit has
    2. A.
    apogee at earth and perigee at Mars.
    B.
    both apogee and perigee at earth.
    C.
    apogee at Mars and perigee at earth.
    D.
    both apogee and perigee at Mars.

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    Answer : Option C

    Explanation :

    -NA-

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