Solving a Fraction: Calculate Velocity of an Orbit

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To calculate the velocity of an orbit at apogee or perigee, the equation involves simplifying the fraction \((x-y)/(x^2-y^2)\). This can be expressed as the difference of squares, allowing for cancellation. The simplification leads to the result that \((x^2-y^2)/(x-y)\) equals \(x+y\), provided \(x-y\) is not zero. Understanding this algebraic manipulation is crucial for deriving the velocity equation. The discussion emphasizes the importance of correctly handling the fraction to achieve the desired outcome in orbital calculations.
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I'm trying to figure out how to calculate the velocity of an orbit at apogee or perigee and I've figured out the derivation of the equation except for this one fraction... I replaced the radius quantities for x and y for ease of viewing.

\frac{x-y}{x^2 - y^2} = \frac{1}{x + y}

Can anybody break this down for me barney-style?
 
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James Brady said:
I'm trying to figure out how to calculate the velocity of an orbit at apogee or perigee and I've figured out the derivation of the equation except for this one fraction... I replaced the radius quantities for x and y for ease of viewing.

\frac{x-y}{x^2 - y^2} = \frac{1}{x + y}

Can anybody break this down for me barney-style?

Express the $$x^2-y^2$$ as the difference of 2 squares.

Then it will cancel to give the right hand fraction.
 
As long as x- y is not equal to 0, (x^2- y^2)/(x- y)= (x- y)(x+ y)/(x- y)= x+ y.
 
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