From One North Pole to the Other

There are two identical uniform spherical planets of radius R R . The first has its center at the origin of the x y z xyz coordinate system. The second has its center at ( x , y , z ) = ( 2 R , 0 , 0 ) (x,y,z) = (2 R,0,0) . The planets are touching.

A projectile is launched from the "North Pole" of the first planet at ( x , y , z ) = ( 0 , 0 , R ) (x,y,z) = (0,0,R) with its initial velocity pointed in the direction of the vector ( 1 , 0 , 1 ) (1,0,1) .

Let the escape speed relative to the planet's surface be v e v_e . Note that here, the escape speed is for a single planet in isolation (following the typical convention).

With the given launch vector, let v 0 v_0 be the minimum launch speed for the projectile to reach the "North Pole" of the second planet at ( x , y , z ) = ( 2 R , 0 , R ) (x,y,z) = (2R,0,R) . The two speeds are related as follows:

v 0 = α v e \large{v_0 = \alpha \, v_e}

Determine the value of α \alpha


The answer is 0.813.

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1 solution

Mark Hennings
Mar 15, 2019

We are being asked to solve the paired differential equations x ¨ = g R 2 [ x ( x 2 + y 2 ) 3 2 + x 2 R ( ( x 2 R ) 2 + y 2 ) 3 2 ] y ¨ = g R 2 [ y ( x 2 + y 2 ) 3 2 + y ( ( x 2 R ) 2 + y 2 ) 3 2 ] \begin{aligned} \ddot{x} & = \; -gR^2\left[\frac{x}{(x^2 + y^2)^{\frac32}} + \frac{x-2R}{((x-2R)^2 + y^2)^{\frac32}}\right] \\ \ddot{y} & = \; -gR^2\left[\frac{y}{(x^2 + y^2)^{\frac32}} + \frac{y}{((x-2R)^2 + y^2)^{\frac32}}\right] \end{aligned} together with the initial conditions x ( 0 ) = 0 x(0) = 0 , y ( 0 ) = R y(0) = R , x ˙ ( 0 ) = y ˙ ( 0 ) = α 2 v e \dot{x}(0) = \dot{y}(0) = \frac{\alpha}{\sqrt{2}}v_e , where, of course, v e = 2 g R v_e = \sqrt{2gR} .

We can render these equations dimensionless by changing variables so that x = R X x = RX , y = R Y y = RY , t = R g T t = \sqrt{\tfrac{R}{g}}T , and the equations become x = [ X ( X 2 + Y 2 ) 3 2 + X 2 ( ( X 2 ) 2 + Y 2 ) 3 2 ] y = [ Y ( X 2 + Y 2 ) 3 2 + Y ( ( X 2 ) 2 + Y 2 ) 3 2 ] \begin{aligned} x'' & = \; -\left[\frac{X}{(X^2 + Y^2)^{\frac32}} + \frac{X-2}{((X-2)^2 + Y^2)^{\frac32}}\right] \\ y'' & = \; -\left[\frac{Y}{(X^2 + Y^2)^{\frac32}} + \frac{Y}{((X-2)^2 + Y^2)^{\frac32}}\right] \end{aligned} with the initial conditions X ( 0 ) = 0 X(0) = 0 , Y ( 0 ) = 1 Y(0) = 1 , X ( 0 ) = Y ( 0 ) = α X'(0) = Y'(0) = \alpha . Here a dash represents differentiation with respect to T T .

Given a particular value of α \alpha , we want to find the first value of T T for which X ( T ) = 2 X(T) = 2 , and determine the corresponding value of Y ( T ) Y(T) . We need to find the value of α \alpha such that Y ( T ) = 1 Y(T) = 1 when first X ( T ) = 2 X(T) = 2 . Searching numerically in the range 0.7 < α < 1 0.7 < \alpha < 1 , we find that the required value of α \alpha is 0.8131305 \boxed{0.8131305}

Is the path traversed by the projectile an ellipse , parabola , circle or neither ? I can only figure out that it is symmetric about the plane passing through the contact point of the planets. Thanks in advance.

Jacob Sony - 2 years, 2 months ago

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I would guess that it is none of these. I doubt that these equations have an exact solution...

Mark Hennings - 2 years, 2 months ago

it will move in ellipse with foci the centre of two planets

Karthik Sai - 2 years ago

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This is not true. The tangents at the ends of the latus rectum of an ellipse have gradient ± e \pm e , where 0 < e < 1 0 < e < 1 is the eccentricity. The path in this question has gradient 1 1 , so the trajectory is not an ellipse as you suggest.

Mark Hennings - 2 years ago

@Mark Hennings How do you reach this differential equation?. And how solved it??
Thanks in advance

A Former Brilliant Member - 1 year, 1 month ago

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