document.write( "Question 4070: Please help I am not sure how to solve the following!\r
\n" ); document.write( "\n" ); document.write( "s=1/2 gt^2 (solve for g)
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Algebra.Com's Answer #1794 by khwang(438)\"\" \"About 
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Let the altitude be h and the radius of the earch be R.
\n" ); document.write( "Also, assume the velociety the of the satellite is V
\n" ); document.write( " the central force mV^2/(R+h) = GmM/(R+h)^2
\n" ); document.write( " or V^2 = GM/(R+h)
\n" ); document.write( " so V = sqrt(GM/(R+h))...(1)
\n" ); document.write( " (where M is the mass of the earth , m is the mass of the satellite
\n" ); document.write( " G is the gravitational constant))
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\n" ); document.write( " The length of the orbit of the satellite is
\n" ); document.write( " 2pi(R+h) = V* 1.5 ( 90 min = 1.5 hrs)
\n" ); document.write( " Solve 2pi(R+h) = 1.5 sqrt(GM/(R+h))...(2)
\n" ); document.write( " for h (by taking squares on both sides) then you can get the answer
\n" ); document.write( " of h(altitude)\r
\n" ); document.write( "\n" ); document.write( " Let T be the time for a satellite to orbit (of radius R+h) the earth.
\n" ); document.write( " Use (1), we have
\n" ); document.write( " T = 2pi (R+h)/ V = 2pi (R+h) /sqrt(GM/(R+h)) = 2pi(R+h)^(3/2)/sqrt(GM)
\n" ); document.write( " so T is an increasing function of h.\r
\n" ); document.write( "\n" ); document.write( " When h = 0, T has min. value 2pi(R)^(3/2)/sqrt(GM).
\n" ); document.write( " But since mg = mGM/R^2 = m V^2/R. (g =9.8 meter/sec^2)
\n" ); document.write( " The corresponding V = sqrt(Rg).
\n" ); document.write( " So, T has min value = 2pi R/ V = 2pi R/ sqrt(Rg) = 2pi sqrt(R/g) \r
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\n" ); document.write( " Of course, you have to find the values of R,M & G by yourself to solve
\n" ); document.write( " (2) and find min T.\r
\n" ); document.write( "\n" ); document.write( " Kenny
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