Posted by sonia on Tuesday, October 7, 2008 at 10:40pm.
You need to derive or find the "rocket" formula for the velocity of an object that has a fixed force T applied while its mass is decreasing. Calculus is needed to derive it.
You can find it at
http://www.ebtx.com/mars/rocketeq.htm
You will need the rocket exhaust velocity, Ve.
You can get if from
T = dm/dt * Ve
where dm/dt is the rate of mass release, 12.7*10^-3 kg/1.90 s,
and T is the thrust in Newtons
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