B https://session.masteringphysics.com/m Physics 1-PHYS 1021 s.com/myct/itemView
ID: 2866966 • Letter: B
Question
Explanation / Answer
E = (1/2)mv^2 - GMm/r = -GMm/(2a)
v^2 = mu ( (2/r) + (1/a) )
mu = GM
r = distance of the orbiting body from primary focus
a = semi major axis of the body's orbit
delta V1 = sqrt ( mu / r1) ( sqrt (2r2 / (r1 + r2 )) - 1)
delta V1 = sqrt ( mu / r2) ( 1- sqrt (2r1 / (r1 + r2 )) )
delta V (total) = delta V1 + delta V2
t(H) = (1/2) sqrt(4*(pi^2)*(a^3) / mu)
t(H) = pi * sqrt{((r1+r2)^3 )/(8*mu)}
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