Results


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Our results show that the values for payload weights to fuel weights, at given exhaust velocities, are linear equations. Thus, we find that the greater the payload, the greater the needed fuel to put the payload in LEO. We have found that the exhaust velocity also greatly affects the fuel weight. However, the exhaust velocity does not affect the fuel proportionally, as the payload does, rather, there is a curve.


The images used were from the fallowing locations:
www.ender-design.com
www.gifanimations.com