Maurice Tutor

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About Maurice Tutor

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Expertise:
Algebra,Applied Sciences See all
Algebra,Applied Sciences,Biology,Calculus,Chemistry,Economics,English,Essay writing,Geography,Geology,Health & Medical,Physics,Science Hide all
Teaching Since: May 2017
Last Sign in: 398 Weeks Ago, 2 Days Ago
Questions Answered: 66690
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Education

  • MCS,PHD
    Argosy University/ Phoniex University/
    Nov-2005 - Oct-2011

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  • Professor
    Phoniex University
    Oct-2001 - Nov-2016

Category > Management Posted 06 Nov 2017 My Price 5.00

value of the constant

(a) Use the substitution v = dy/dt to solve (13) for v in terms of y. Assume that the velocity of the rocket at burnout is v = v0 and that y ≈ R at that instant; show that the approximate value of the constant c of integration is

(b) Use the solution for v in part (a) to show that the escape velocity of the rocket is given by v0Take y →∞ and assume v > 0 for all time t.]

(c) The result in part (b) holds for any body in the solar system. Use the values g = 32 ft/s2 and R = 4000mi to show that the escape velocity from the Earth is (approximately) V0= 25,000 mi/h.

(d) Find the escape velocity from the Moon if the acceleration of gravity is 0.165g and R = 1080 mi.

 

Answers

Maurice Tutor
(5)
Status NEW Posted 06 Nov 2017 09:11 PM My Price 5.00

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