AAWSAP DIRD, Aneutronic Fusion Propulsion I, November 2010

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Figure 13. Maximum Achievable Velocity Versus Fuel Usage.
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Figure 14. Acceleration and Rocket "Clock" Ratio versus Mission Time on Earth.
Another item to consider is the value chosen for the constant acceleration of the
spacecraft. We cannot exceed 1 g for crew safety, yet higher accelerations mean
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