On what does gravity assist depend? (possibly with sources)

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    Orbital mecahnics
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SUMMARY

The discussion centers on the factors affecting gravity assist maneuvers in space exploration. Key elements include the velocity of the probe, the angle of attack, and the relative motion between the probe and the planet. The participants emphasize that the probe must pass behind the planet to gain velocity in the planet's direction and in front to gain velocity away from it. Understanding these dynamics is crucial for optimizing trajectory design in missions involving gravity assists.

PREREQUISITES
  • Understanding of orbital mechanics
  • Familiarity with hyperbolic orbits
  • Knowledge of velocity change in gravitational interactions
  • Basic principles of spacecraft navigation
NEXT STEPS
  • Research "Orbital Mechanics for Engineering Students" by Howard D. Curtis
  • Study "Gravity Assist Maneuvers" in NASA's Jet Propulsion Laboratory resources
  • Explore simulations of gravity assists using tools like GMAT (General Mission Analysis Tool)
  • Learn about the "Hohmann Transfer Orbit" and its applications in mission planning
USEFUL FOR

Aerospace engineers, astrophysicists, students in space science, and anyone involved in mission planning for interplanetary travel will benefit from this discussion.

renobueno
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Thread moved from the technical forums to the schoolwork forums
Hey guys, I am preparing for a presentation about gravity assist and I cant find much information about this topic. Ive gone already through wikipedia but wikipedia only talks about the velocity change. What are other factors which could have affects on the gravity assist?

Like I assume the velocity of the probe is important and perhaps even the angle of attack. But I couldnt explain why.

Hope you can help me out! I've searching for valuable sources for the past 6h but couldnt find something between oversimplified and raw physics degree. :(
 
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It is just a velocity change, though, isn't it? Looking at the planet and the probe, they just loop round each other in a hyperbolic orbit, and they both change speed and direction (the probe more than the planet, due to the mass ratio). You just set up the approach to the planet so the exit speed of the probe is faster with respect to the Sun (or slower, whichever you were going for).

What education level are you supposed to be presenting at?
 
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A key aspect to explain is why you need to pass behind the planet to gain velocity in the planet's direction but in front of it to gain velocity the other way.
Can you find an argument for that?
 
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