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

Source URL: www.icarusinterstellar.org

• Aerospace engineering
• Physics
• Escape velocity
• Rocket
• Specific orbital energy
• Kinetic energy
• Orbit
• DaVinci3
• Parabolic trajectory
• Astrodynamics
• Celestial mechanics
• Space technology