Math 2.0

Mechanics of particles and systems Definition

Gravity assist

Builds on Patched conic approximationKepler orbitHyperbola

Definition

Work in the patched conic approximation. Let a planet with gravitational parameter μ>0\mu > 0 move with velocity VV relative to the Sun, taken as constant during the flyby. A spacecraft enters the planet's sphere of influence with velocity vinv_{\mathrm{in}} relative to the Sun. Inside it moves on a hyperbolic Kepler orbit about the planet, with arrival velocity uin=vin−Vu_{\mathrm{in}} = v_{\mathrm{in}} - V relative to the planet and periapsis distance rp>0r_p > 0. It leaves with velocity uoutu_{\mathrm{out}} relative to the planet, where ∥uout∥=∥uin∥=v∞\norm{u_{\mathrm{out}}} = \norm{u_{\mathrm{in}}} = v_\infty and the angle δ\delta between uinu_{\mathrm{in}} and uoutu_{\mathrm{out}} satisfies sin⁡δ2=1e,e=1+rpv∞2μ.\sin \frac{\delta}{2} = \frac{1}{e}, \qquad e = 1 + \frac{r_p v_\infty^2}{\mu}. The change of heliocentric velocity vout−vin=uout−uinv_{\mathrm{out}} - v_{\mathrm{in}} = u_{\mathrm{out}} - u_{\mathrm{in}}, with vout=V+uoutv_{\mathrm{out}} = V + u_{\mathrm{out}}, is the gravity assist.

Remarks

The size of the change is ∥uout−uin∥=2v∞sin⁡(δ/2)\norm{u_{\mathrm{out}} - u_{\mathrm{in}}} = 2 v_\infty \sin(\delta/2). The heliocentric speed changes because ∥V+uout∥\norm{V + u_{\mathrm{out}}} differs from ∥V+uin∥\norm{V + u_{\mathrm{in}}} in general. It grows when the craft passes behind the planet, so that uoutu_{\mathrm{out}} turns towards VV.

Example: let uu be parallel to VV with ∥u∥=v∞\norm{u} = v_\infty, and let uin=−uu_{\mathrm{in}} = -u and uout=uu_{\mathrm{out}} = u. Then the heliocentric speed goes from ∥V∥−v∞\norm{V} - v_\infty to ∥V∥+v∞\norm{V} + v_\infty, a gain of 2v∞2 v_\infty. This is the limit δ→π\delta \to \pi, which needs rp→0r_p \to 0.

Non-example: if the attracting body does not move, V=0V = 0, then ∥vout∥=∥vin∥\norm{v_{\mathrm{out}}} = \norm{v_{\mathrm{in}}}, so the flyby only turns the craft and its speed relative to the body is unchanged.

The total energy of the craft and the planet is conserved; the planet's change of speed is negligible because of its large mass.

Reading path

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  1. Hyperbola concept
  2. Kepler orbit concept
  3. Patched conic approximation concept
  4. Gravity assist definition

Further reading

  1. Web https://en.wikipedia.org/wiki/Gravity_assist
About this page
Tag51CJVWZPY6
URIm2://51CJVWZPY6
Kinddefinition
WritingW0 stub
MSC70M20, 70F15
DefinesGravity assist
UsesPatched conic approximation, Kepler orbit, Hyperbola
Changed3 November 2026

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