Using Venus in the Parker Solar Probe mission

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SUMMARY

The Parker Solar Probe mission will utilize gravity assists from Venus to progressively lower its orbit towards the Sun over a span of seven years. The probe will execute seven flybys of Venus, strategically passing "in front" of the planet to reduce its orbital energy, akin to the effect of retro rockets. This maneuver allows the probe to accelerate Venus slightly while simultaneously enabling the probe to fall into a smaller orbit around the Sun. The discussion clarifies the mechanics of this gravity assist and its implications for orbital dynamics.

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  • Understanding of gravity assist maneuvers in orbital mechanics
  • Familiarity with the concepts of kinetic and potential energy in space travel
  • Knowledge of the Parker Solar Probe mission objectives and timeline
  • Basic principles of celestial mechanics and orbital dynamics
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  • Research "gravity assist techniques in space missions" for deeper insights
  • Study "orbital mechanics and energy transfer" to understand energy changes during flybys
  • Explore "Parker Solar Probe mission details" for updates on its progress and findings
  • Investigate "retro rocket propulsion methods" for comparison with gravity assists
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Aerospace engineers, astrophysicists, and space mission planners will benefit from this discussion, particularly those interested in orbital mechanics and the specifics of the Parker Solar Probe mission.

sophiecentaur
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The Parker Solar Probe mission will be launched soon and I was reading that it will use gravity assist from Venus to bring its orbit closer and closer to the Sun over about seven years.
The diagram in this link shows the plan for seven flyby's of Venus to lower the orbit. Now, to get down close to the Sun, the probe needs to lose potential energy so , unlike with space shots that take probes to outer planets, where the probes acquire Kinetic Energy on their flyby's, the probe's orbital energy needs to be reduced. So it looks like the probe needs to pass Venus 'on the other side' so that it accelerates Venus and slows down the probe, just as if it were using retro rockets.
Can someone confirm this or put me right on the details, please?
 
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I'm bumping this because it strikes me as a topic worth discussing - when you read so many comments about getting out of the Solar system using the same method.
I'm wondering about posting a similar question in General Physics.
 
sophiecentaur said:
The Parker Solar Probe mission will be launched soon and I was reading that it will use gravity assist from Venus to bring its orbit closer and closer to the Sun over about seven years.
The diagram in this link shows the plan for seven flyby's of Venus to lower the orbit. Now, to get down close to the Sun, the probe needs to lose potential energy so , unlike with space shots that take probes to outer planets, where the probes acquire Kinetic Energy on their flyby's, the probe's orbital energy needs to be reduced. So it looks like the probe needs to pass Venus 'on the other side' so that it accelerates Venus and slows down the probe, just as if it were using retro rockets.
Can someone confirm this or put me right on the details, please?

The figure is not helpful for your questions, but you are correct. In Venus's frame, the probe accelerates it slightly by passing "in front" of Venus on the probe's path to the inner Solar System and pulls it to a higher orbit. "In front" here means, in the direction of Venus's instantaneous orbital velocity -- let's say, for concreteness, that means between Venus and Antares at that moment.

Conversely, in the probe's frame, by passing between Venus and Antares (they agree on the geometry when expressed this way!), the probe experiences an acceleration that sends it more directly toward the Sun. Even though its asymptotic speed [that is, pre & post-encounter] relative to Venus does not change, it has given Venus some of its orbital energy and "falls" into a smaller orbit about the Sun.
 
JMz said:
it has given Venus some of its orbital energy and "falls" into a smaller orbit
I guess that's oneway of describing what goes on. But, if there is just a change of direction, with no loss of speed (KE), then where is the equivalent action of a retro rocket which is the more common way of dropping down an orbit?
The retro rocket method involves a (-KE) burst whilst at apogee to reduce orbital energy. Your interpretation implies a change in position, after passing by Venus. That's hard to visualise but I could be convinced, I suppose.
PS I take your point about the usefulness of the diagram but it's all I could get hold of.
 
@JMz I just re read your post and I had missed out the Frame of Venus bit. Its KE is not changed in that frame but are we not concerned by the KE change in the Sun's Frame?
I don't think this needs to be pursued much further as I am getting the idea now.
Cheers.
 

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