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Gravity Assist (Slingshot)

Also known as: Gravitational Slingshot, Flyby, Gravity Slingshot

📘 Definition
A gravity assist — also called a gravitational slingshot or planetary swingby — is a manoeuvre in which a spacecraft flies close to a planet or moon to gain or lose speed relative to the Sun, using the body's gravity instead of propellant. The trick is one of reference frames: in the planet's frame the craft swings past on a hyperbolic path and departs at exactly the speed it arrived with, only redirected. But the planet is itself racing around the Sun, so adding that orbital motion back in turns the change of direction into a change of Sun-relative speed. Pass behind the planet and the craft is flung forward; pass in front and it is slowed. The energy is borrowed, not created — the planet is nudged in its own orbit by an immeasurably tiny amount. This propellant-free delta-v let Voyager 2 chain flybys of Jupiter, Saturn and Uranus to reach Neptune, far more cheaply than a direct route could (compare the Hohmann transfer).
Zero (trajectory only)
Propellant cost
Up to ~10 km/s (Jupiter)
Speed change
≈2× planet's orbital speed
Theoretical max
Voyager 2 Grand Tour
Classic mission

Understanding Gravity Assist

Why the spacecraft speeds up: the reference-frame trick

The apparent paradox — that a craft can leave a flyby faster while its speed relative to the planet never changes — dissolves once you pick the right frame. Relative to the planet, a gravity assist is just a hyperbolic flyby: the craft comes in, whips around and leaves at identical speed but with a rotated velocity vector. Energy relative to the planet is conserved. Switch to the Sun's frame, however, and you must add the planet's own orbital velocity (about 13 km/s for Jupiter, 30 km/s for Earth). Rotating the craft's velocity so it points more along the planet's direction of travel means a larger Sun-relative speed on the way out. The gain is real kinetic energy, drawn from the planet's orbital motion; because a planet outmasses a probe by a factor of roughly 10^24, its own slowdown is utterly unmeasurable. It is the same physics that reshapes the orbits of near-Earth objects when they pass close to a planet.

It can slow a craft down, too

A gravity assist is not only an accelerator. Approach a planet on its leading side — in front of its motion — and the encounter drains Sun-relative speed instead of adding it. Missions heading sunward exploit exactly this. NASA's Parker Solar Probe used seven Venus gravity assists between 2018 and 2024 to shed orbital energy and tighten its loops around the Sun, closing to about 6.1 million km (3.8 million miles) from the solar surface on 24 December 2024 while travelling near 692,000 km/h — the fastest craft ever built. Whether a flyby adds or removes energy depends only on the geometry of the approach, which is why mission designers treat the planets as a set of free, if inflexible, velocity-change stations.

Famous gravity-assist missions

From the outer planets to the Sun itself, gravity assists have flown missions that no rocket of their era could have reached directly.

Mission (launch)Assist sequenceDestinationPayoff
Voyager 2 (1977)Jupiter → Saturn → UranusNeptuneOnly craft to visit all four giant planets; rode an alignment recurring roughly every 175 years
Cassini (1997)Venus → Venus → Earth → JupiterSaturnReached Saturn with a launcher far too small for a direct flight
New Horizons (2006)JupiterPluto & Kuiper BeltJupiter flyby added about 4 km/s, cutting roughly 3 years off the trip
Parker Solar Probe (2018)Venus × 7Sun's coronaShed energy to close within about 6.1 million km of the Sun

The catch: 'free' but tightly constrained

The propellant saving is genuine, but a gravity assist buys it with time and rigidity. The assisting planet has to be in the right place at the right moment, so launch windows can be narrow and rare; the Voyagers rode a planetary alignment that will not repeat for well over a century. Chained flybys can also add years of cruise time compared with a direct burn, and navigation must be precise to the kilometre, since a small error at closest approach multiplies downstream. Engineers sometimes combine an assist with a rocket burn deep in the planet's gravity well — a powered, or Oberth, flyby — to squeeze out extra energy, a different lever from the efficiency measured by specific impulse. Even so, for the outer Solar System the sums are decisive: no chemical rocket ever built could carry enough fuel to reach Neptune the direct way in a comparable time.

🛰️ See the physics in the wild
A deliberate gravity assist is the engineered version of something nature does constantly: when an asteroid passes close to a planet, that planet's gravity bends its path and shifts its speed around the Sun. Watch real planetary close approaches on our near-Earth object tracker.
Open the NEO tracker →
📖 Learn More

Frequently Asked Questions

Correct — a gravity assist uses no propellant at all; the energy comes from the planet's orbital motion around the Sun, not from the spacecraft's engines, making a flyby essentially free delta-v. The trade-off is that the planet must be in exactly the right position, so the technique constrains launch windows and often lengthens the journey rather than shortening it. Small trajectory-correction burns are still needed to aim the flyby precisely.
Because speed relative to the planet and speed relative to the Sun are two different things. In the planet's frame the craft leaves a flyby at the same speed it entered, only redirected. But the planet is orbiting the Sun at tens of kilometres per second, so once you add that motion back in, the change of direction becomes a change of Sun-relative speed. The kinetic energy gained is taken from the planet's orbit, which slows by an unmeasurably small amount.
Yes. Whether a flyby adds or removes speed depends purely on geometry: pass behind the planet's direction of travel and you gain Sun-relative speed, pass in front and you lose it. Missions bound for the inner Solar System rely on this — NASA's Parker Solar Probe used seven Venus flybys to shed orbital energy and spiral closer to the Sun, reaching about 6.1 million km from the solar surface in December 2024.
A gravity assist changes a spacecraft's Sun-relative velocity by borrowing momentum from a planet and uses no fuel, whereas the Oberth effect is the extra efficiency a rocket gains by burning fuel while moving fast deep in a gravity well. They are often combined in a 'powered flyby', firing the engine at closest approach, but they remain distinct: one is propellant-free trajectory design, the other is a way to make a burn go further.
Because no rocket could carry enough fuel to fly directly to Neptune in a reasonable time. A rare alignment of Jupiter, Saturn, Uranus and Neptune in the late 1970s — one that recurs only about every 175 years — let Voyager 2 chain a flyby of each planet, each one flinging it onward to the next. Without those assists the outer-planet 'Grand Tour' would have been impossible with the technology of the day.
It depends on the planet's mass and orbital velocity. A single Jupiter flyby can change a spacecraft's Sun-relative speed by up to roughly 10 km/s, as the Voyagers experienced. The theoretical ceiling for one encounter is about twice the planet's own orbital speed, though real flybys fall well short because the bending angle is limited by how close the craft can safely pass. Chaining several planets multiplies the total effect.

Sources & References

Definitions are reviewed against primary sources. Last reviewed: 2026-08-24.