Date: 2011-07-05 01:47:25Aerospace 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 AdministrationAdd to Reading ListSource URL: www.icarusinterstellar.orgDownload Document from Source Website File Size: 542,04 KBShare Document on Facebook
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