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Unformatted text preview: time after launch, if the rocket experiences a drag force (force of air resistance) opposing its motion that is equal to: 2 2 1 R D D V C F ρ = Here, C D is the drag coefficient. Assume an isothermal model for the atmosphere to model the variation in atmospheric air density with altitude. Put these equations into forms firstorder (in time) for rocket velocity V R , mass, M, and height, h. PROBLEM SET 5 SOLUTIONS PROBLEM SET 5 SOLUTIONS PROBLEM SET 5 SOLUTIONS PROBLEM SET 5 SOLUTIONS PROBLEM SET 5 SOLUTIONS PROBLEM SET 5 SOLUTIONS PROBLEM SET 5 SOLUTIONS PROBLEM SET 5 SOLUTIONS...
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This note was uploaded on 08/01/2009 for the course ME 70 taught by Professor Cappelli,m during the Winter '08 term at Stanford.
 Winter '08
 Cappelli,M

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