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OALib Journal期刊
ISSN: 2333-9721
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Escape Velocity

DOI: 10.5038/2326-3652.3.1.24

Keywords: Escape Velocity , Single Staged Rocket , Kinetic Energy

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Abstract:

In this project, we investigated if it is feasible for a single staged rocket with constant thrust to attain escape velocity. We derived an equation for the velocity and position of a single staged rocket that launches vertically. From this equation, we determined if an ideal model of a rocket is able to reach escape velocity.

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