pridet8
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Homework Statement
A rocket engine has an exhaust velocity of 20,000 m/sec. The mass flow (dm/dt) rate is 1 milligram per second.
a) What is the thrust produced by the engine?
b) The engine propels a 200 kg space craft. What change in velocity is achievable by running the engine continuously for one solid year?
note1: assume a constant mass for the system.
note2: One year = 31.56 x 10^6 seconds.
Homework Equations
Thrust = -Ve*(dm/dt)
Change in velocity = V - Vo = Ve*(ln Mo/M)
The Attempt at a Solution
a) Thrust = 20000m/s *(.000001kg/s) = .02N
b) 20000*(ln 200kg/31.56kg) = 36928.6 m/s^2
My question: Part A I believe is right but part b I am having trouble believing. Should I just keep it simple since the mass is constant at 200 kg? Thus giving a new equation which would be
a = (Thrust - W)/M
which is (.02N - (200kg*9.8m/s2))/200kg = 9.79m/s^2