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How do probes use gravity boosts to leave Earth and reach other planets?

Research question: How do today's deep-space probes use gravity assists to leave Earth's orbit and head for other planets?

The records show that a gravity assist changes a probe's heading without changing its speed relative to the planet 9, and that its speed relative to the Sun changes because it is the vector sum of its speed relative to the planet and the planet's orbital speed 12. JUICE, launched on April 14, 2023, is in an 8-year cruise to Jupiter that relies on gravity assists from Venus, Earth, and the Moon 3, and it completed the first Lunar-Earth gravity assist in August 2024 6. The records show that a planetary flyby's turn angle is limited by the planet's minimum flyby altitude, about 65 degrees for Mars 5, and that meeting the excess-speed threshold is necessary but not sufficient, since the incoming direction must also fall within the planet's deflection cone 7. The facts do not explain specifically how today's probes leave Earth's orbit, and the newest fact dates from 2026 1.

Checked 2026-10-18. Only documented and supported facts are used.
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Sources

[1] supported
A gravity assist cannot change the magnitude of a spacecraft's hyperbolic excess speed, because an unpowered flyby preserves it, so the energy requirement is set before the encounter.
"an energetic penalty that is fixed before the encounter because an unpowered flyby preserves the magnitude of the excess velocity."
A Tisserand-Based Reachability Criterion for Gravity-Assist Selection: Why a Single Venus Flyby Is Ineffective for Rendezvous with (16) Psyche (2026)
[2] supported
Single planetary flybys alone do not explain NASA's Psyche mission; its trajectory relies on low-thrust propulsion rather than any single impulsive flyby.
"they explain why low-thrust propulsion—rather than any single impulsive flyby—underpins the trajectory of NASA’s Psyche mission."
A Tisserand-Based Reachability Criterion for Gravity-Assist Selection: Why a Single Venus Flyby Is Ineffective for Rendezvous with (16) Psyche (2026)
[3] supported
JUICE launched on April 14, 2023, and is in an 8-year cruise phase to Jupiter that relies on gravity assists from Venus, Earth, and the Moon.
"Launched on April 14, 2023, JUICE is currently in an 8-year cruise phase to Jupiter, utilizing gravity assists from Venus, Earth, and the Moon."
Estimation of Spacecraft Outgassing During the Lunar-Earth Gravity Assist of JUICE Using Radiometric Observations  (2025)
[4] supported
After the lunar gravity assist, Juice approached Earth from the magnetotail and entered the plasmasphere before its Earth closest approach.
"Following the lunar gravity assist, Juice approached from the magnetotail and entered the plasmasphere."
Spacecraft charging during the 2024 Juice Earth gravity assist (2025)
[5] supported
A gravity assist can only redirect a probe's velocity by a limited turn angle set by the planet's minimum flyby altitude, and for Mars this is about 65 degrees, which was insufficient for a Psyche transfer.
"far exceeding the ≈65° that Mars can deliver at its minimum allowable flyby periapsis, defined as the planetary mean radius plus a 250 km altitude margin."
A Tisserand-Based Reachability Criterion for Gravity-Assist Selection: Why a Single Venus Flyby Is Ineffective for Rendezvous with (16) Psyche (2026)
[6] supported
JUICE was the first spacecraft to perform a Lunar-Earth gravity assist (LEGA), which was completed in August 2024.
"Notably, JUICE is the first spacecraft to execute a Lunar-Earth gravity assist (LEGA), which was successfully completed in August 2024."
Estimation of Spacecraft Outgassing During the Lunar-Earth Gravity Assist of JUICE Using Radiometric Observations  (2025)
[7] supported
Meeting the required excess-speed threshold is necessary but not sufficient for a gravity assist; the incoming velocity direction must also fall within the planet's attainable deflection cone.
"satisfying the scalar criterion is necessary but not sufficient: the excess-velocity vector delivered by the inbound leg must also lie within the attainable deflection cone of the assisting planet"
A Tisserand-Based Reachability Criterion for Gravity-Assist Selection: Why a Single Venus Flyby Is Ineffective for Rendezvous with (16) Psyche (2026)
[8] supported
The lunar gravity assist gave JUICE a critical trajectory adjustment and also let several onboard instruments operate during the flyby.
"This maneuver provided a critical trajectory adjustment while also allowing several onboard instruments to operate during the flyby."
Estimation of Spacecraft Outgassing During the Lunar-Earth Gravity Assist of JUICE Using Radiometric Observations  (2025)
[9] supported
A gravity assist changes a probe's heading without changing its speed relative to the planet, because the probe leaves the planet with the same speed it arrived with.
"Vom Planeten aus gesehen verlässt die Raumsonde ihn mit derselben Geschwindigkeit, mit der sie auf ihn traf, d. h. die Bahnenergie des Raumfahrzeugs bezogen auf den Planeten bleibt konstant."
Swing-by
[10] supported
The document says that once a spacecraft leaves Earth's Hill sphere it usually becomes a solar orbiter, which is how departing probes enter heliocentric orbit.
"Sobald ein Raumflugkörper die Hill-Sphäre der Erde verlässt, wird er im Regelfall zu einem Sonnenorbiter."
Orbitalflug
[11] supported
The original BepiColombo plan called for launch in 2009–2010 with about three years of flight time, using electric propulsion and several gravity assists.
"Die Mission sah ursprünglich einen Start mit zwei Orbitern zwischen 2009 und 2010 und drei Jahre Flugzeit mit elektrischem Antrieb und mehreren Gravity-Assists vor."
BepiColombo
[12] supported
The probe gains or loses speed relative to the Sun because its speed relative to the Sun is the vector sum of its speed relative to the planet and the planet's own orbital speed around the Sun, and that sum changes in magnitude.
"Die Geschwindigkeit der Sonde relativ zur Sonne ist die vektorielle Summe der Geschwindigkeit der Sonde relativ zum Planeten und der Geschwindigkeit des Planeten um die Sonne, und diese Summe ändert sich im Betrag."
Swing-by
[13] supported
The document says a spacecraft can use a swing-by maneuver past another celestial body to reduce its speed, and that this usually still requires further engine burns to reach the final orbit.
"Man kann auch treibstoffsparend die Atmosphäre des Himmelskörpers (wenn vorhanden) für eine Atmosphärenbremsung benutzen oder vorab durch ein Swing-by -Manöver an einen weiteren Himmelskörper die Geschwindigkeit reduzieren. Hierbei sind aber gewöhnlich weitere Manöver mit einem Triebwerk nötig, um die finale Bahn zu erreichen."
Orbitalflug
[14] supported
BepiColombo's route to Mercury includes a series of Mercury swing-bys, the second of which was scheduled for 23 June 2022.
"Datum=23.06.2022 |Text=2. Swing-by am Merkur"
BepiColombo
[15] supported
Jupiter was intended to serve as a 'slingshot' to let probes reach Saturn, Uranus, Neptune and Pluto in an acceptable time.
"Jupiter sollte als „Sprungbrett“ dienen, um die Planeten Saturn , Uranus , Neptun und Pluto in akzeptabler Zeit zu erreichen"
Voyager-Programm
[16] supported
Voyager 2 only reached the Sun's escape velocity after a gravity assist at Jupiter.
"Erst durch Swing-by am Jupiter konnte die Flucht"
Swing-by
[17] supported
The mission's swing-by schedule at Mercury runs from the 1st through the 6th flyby, with the sixth scheduled for 8 January 2025.
"Datum=08.01.2025 |Text=6. Swing-by am Merkur"
BepiColombo
[18] supported
Gary Flandro, also at JPL, calculated flight paths that exploited the favorable alignment of the outer planets in the late 1970s.
"Drei Jahre später berechnete der Ingenieur Gary Flandro, ebenfalls beim JPL, einige Flugbahnen für Sonden, die die günstigen Stellungen der äußeren Planeten Ende der 1970er Jahre ausnutzen sollten."
Voyager-Programm
[19] supported
The Parker Solar Probe uses seven flybys of Venus to slow down.
"die Parker Solar Probe (2018) nutzt sieben Vorbeiflüge an der Venus zum Abbremsen."
Swing-by
[20] supported
Between 1976 and 1978 the possible gravity-assist routes were Jupiter–Saturn–Uranus–Neptune, Jupiter–Saturn–Pluto, and Jupiter–Uranus–Neptune.
"Zwischen 1976 und 1978 waren folgende Routen möglich: Jupiter–Saturn–Uranus–Neptun, Jupiter–Saturn–Pluto und Jupiter–Uranus–Neptun."
Voyager-Programm
[21] supported
The Rosetta mission reached comet Churyumov–Gerasimenko using several swing-by maneuvers at Earth and Mars.
"Die Rosetta-Mission (2004) erreichte über mehrere Swing-by-Manöver an Erde und Mars den Kometen Tschurjumow-Gerassimenko"
Swing-by
[22] supported
NASA did not want to miss this opportunity because such a favorable planetary alignment would not recur for 176 years.
"Diese Chance wollte sich die NASA nicht entgehen lassen, da sich eine solch günstige Planetenkonstellation erst 176 Jahre später wiederholen wird."
Voyager-Programm