Gravity assist
Top View
- Escape Maneuvers Using Double Lunar Gravity Assist
- Optimal Triangular Lagrange Point Insertion Using Lunar Gravity Assist
- Double Jupiter Gravity Assist for Achieving High Heliocentric Asymptotic Escape Speeds and Missions to Interstellar Objects
- Optimization of Low-Thrust Gravity Assist Trajectories Under Application of Tisserand’S Criterion
- Using Gravity Assist Maneuver to Increase Fuel Consumption Efficiency for a Space Probe Entering Jupiter’S Orbit
- A Historical Review of the Theory of Gravity-Assists in the Pre-Spaceflight
- Interplanetary Transfers, Which Are Optimal with Respect to Fuel Consumption
- Swarm Mission Design in High Altitude Orbit for Heliophysics
- Gravity-Assist Trajectories to Venus, Mars, and the Ice Giants: Mission Design with Human and Robotic Applications Kyle M
- Part Iii : Space Transportation, Propulsion and Pathway Options
- AAE 450 Spacecraft Design Fall 2003, Option 2 Aero-Gravity-Assist Vehicle for Jupiter Mission
- Using the Two-Burn Escape Maneuver for Fast Transfers in the Solar System and Beyond
- Mars Molniya Orbit Atmospheric Resource Mining
- Capturing Near-Earth Asteroids Into Bounded Earth Orbits Using Gravity Assist
- Gravity Assist Preliminary Research & Design
- Technical Appendix
- Interplanetary Gravity Assisted Trajectory Optimizer (IGATO)
- Analysis About Constraints for Low-Thrust Gravity-Assist Sequencing