Two-Burn Escape Maneuver for High DV Capable Spacecraft Robert Adams, Ph.D. Advanced Concepts Office George C. Marshall Space Flight Center National Aeronautics and Space Administration

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Date: 2011-07-05 01:47:25 Aerospace engineering Physics Escape velocity Rocket Specific orbital energy Kinetic energy Orbit DaVinci3 Parabolic trajectory Astrodynamics Celestial mechanics Space technology		Two-Burn Escape Maneuver for High DV Capable Spacecraft Robert Adams, Ph.D. Advanced Concepts Office George C. Marshall Space Flight Center National Aeronautics and Space Administration Add to Reading List Source URL: www.icarusinterstellar.org Download Document from Source Website File Size: 542,04 KB Share Document on Facebook

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