Plymouth Rock: An Early Human Asteroid Mission Using Orion
Plymouth Rock: An Early Human Asteroid Mission Using Orion
Plymouth Rock: An Early Human Asteroid Mission Using Orion
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Launch Vehicle Needs<br />
• <strong>Orion</strong>-based asteroid missions require launch of<br />
about 46 tons to C3 = +1 to +4 km 2 /s 2 (slightly faster<br />
than escape velocity)<br />
– This is roughly equivalent to launching 50-65 mt to trans-<br />
lunar injection (C3 = -1.8 km 2 /s 2 ) depending on the launch<br />
approach<br />
– This could be achieved using several possible launch<br />
architectures<br />
– The planned Ares V capability has margin for this mission<br />
– Ares I performance (in combination with Ares V) is<br />
sufficient for some launch opportunities, but increased<br />
performance would allow <strong>Orion</strong> propellant tanks to be fully<br />
loaded, enabling more opportunities and reducing mission<br />
duration<br />
• <strong>Asteroid</strong> missions using <strong>Orion</strong> and Ares are mainly<br />
limited by factors other than launch, such as reentry<br />
velocity and spacecraft propulsion<br />
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