Physics

Physics

Problem

The perihelion distance rpr_p of a planet in an elliptical orbit of semi-major axis aa and eccentricity ee is a) a(1+e)a(1+e) b) a(1−e2)a(1-e^{2}) c) a(1−e)a(1-e) d) a1+e\dfrac{a}{1+e}

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