Posted by beavis on Wednesday, February 15, 2012 at 5:04pm.
The rocket weight is
M = (1100 - 20 t)*g = 10,780 - 196*t newtons
That equals the thrust when
196*t = 780 N
t = 3.98 seconds
Rockets acclerate during each stage because the thrust stays the same while the mass decreases (until burnout, when the fuel of that stage is gone).
ahh thank you so much!
can you write the actual formulas that you've used because im not sure if i understood it correctly
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