Why do we need the hyperbolic excess velocity?

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SUMMARY

The hyperbolic excess velocity (VHE) is defined by the formula VHE = √(μ/a), where μ represents the standard gravitational parameter and a is the semi-major axis of the transfer orbit. This concept is crucial for understanding interplanetary transfers, particularly in relation to the sphere of influence (RSOI = R(μplanetsun)2/5), which helps in calculating the gravitational effects of celestial bodies. The rationale behind these terms lies in their utility for patched-conic models, which simplify the analysis of trajectories involving multiple celestial bodies.

PREREQUISITES
  • Understanding of orbital mechanics
  • Familiarity with the vis-viva equation
  • Knowledge of gravitational parameters (μ)
  • Concept of sphere of influence (RSOI)
NEXT STEPS
  • Study the vis-viva equation in detail
  • Explore patched-conic approximation techniques
  • Learn about gravitational parameters for various celestial bodies
  • Investigate the implications of sphere of influence in astrodynamics
USEFUL FOR

Aerospace engineers, astrophysicists, and students of orbital mechanics will benefit from this discussion, particularly those involved in mission planning for interplanetary transfers.

TimeRip496
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$$V_{HE}=\sqrt{\frac{\mu}{a}}$$

What is the rationale for this formula when we can determine the change in velocity from Earth's orbit to transfer orbit using the vis-viva equation? Likewise, what is the use of defining the radius for the sphere of influence for interplanetary transfer?
$$R_{SOI}=R(\frac{\mu_{planet}}{\mu_{sun}})^{2/5}$$

I just don't understand the rationale with coming up with these terms when the delta v for the transfer can be determined by finding the velocity from initial, transfer and final orbit.
 
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TimeRip496 said:
$$V_{HE}=\sqrt{\frac{\mu}{a}}$$

What is the rationale for this formula when we can determine the change in velocity from Earth's orbit to transfer orbit using the vis-viva equation? Likewise, what is the use of defining the radius for the sphere of influence for interplanetary transfer?
$$R_{SOI}=R(\frac{\mu_{planet}}{\mu_{sun}})^{2/5}$$

I just don't understand the rationale with coming up with these terms when the delta v for the transfer can be determined by finding the velocity from initial, transfer and final orbit.
Calculations involving sphere of influence are useful for patched-conic models - these are easiest way to analyze multiple-bodies trajectories.
 

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