- Gravity assist
orbital mechanicsand aerospace engineering, a gravitational slingshot, gravity assist or swing-by is the use of the relative movement and gravityof a planetor other celestial body to alter the path and speed of a spacecraft, typically in order to save fuel, time, and expense. Gravity assist can be used to decelerate a spacecraft or accelerate a spacecraft.
Historical origins of the method
In his paper “Тем кто будет читать, чтобы строить” [To whomsoever will read [this paper] in order to build [an interplanetary rocket] , [Kondratyuk’s paper is included in the book: Mel’kumov, T. M., ed., "Pionery Raketnoy Tekhniki" [Pioneers of Rocketry: Selected Papers] (Moscow, U.S.S.R.: Institute for the History of Natural Science and Technology, Academy of Sciences of the USSR, 1964). An English translation of Kondratyuk’s paper was made by NASA. See: NASA Technical Translation F-9285, pages 15-56 (Nov. 1, 1965).] which he dated “1918-1919,” [In 1938, when Kondratyuk submitted his manuscript “To whomsoever will read in order to build” for publication, he dated the manuscript “1918-1919,” although it was apparent that the manuscript had been revised at various times. See page 49 of NASA Technical Translation F-9285 (Nov. 1, 1965).]
Yuri Kondratyuksuggested that a spacecraft traveling between two planets could be accelerated at the beginning of its trajectory and decelerated at the end of its trajectory by using the gravity of the two planets' moons.
In his 1925 paper “Проблема полета при помощи реактивных аппаратов: межпланетные полеты” [Problems of flight by jet propulsion: interplanetary flights] , [Zander‘s 1925 paper, “Problems of flight by jet propulsion: interplanetary flights,” was translated by NASA. See NASA Technical Translation F-147 (1964); specifically, Section 7: Flight Around a Planet’s Satellite for Accelerating or Decelerating Spaceship, pages 290-292.]
Friedrich Zandermade a similar argument.
However, neither investigator realized that gravitational assists from planets "along" a spacecraft’s trajectory could propel a spacecraft and that therefore such assists could greatly reduce the amount of fuel required to travel among the planets. [See page 13 of: Dowling, Richard L.; Kosmann, William J.; Minovitch, Michael A.; and Ridenoure, Rex W., “The origin of gravity-propelled interplanetary space travel” (IAA paper no. 90-630), presented at the 41st Congress of the International Astronautical Federation, which was held 6-12 October 1990 in Dresden, G.D.R. Available on-line at: http://www.gravityassist.com/IAF1/IAF1.pdf .] That discovery was made by
Michael Minovitchin 1961. [Minovitch, Michael, "A method for determining interplanetary free-fall reconnaissance trajectories," Jet Propulsion Laboratory Technical Memo TM-312-130, pages 38-44 (23 August 1961).]
The gravity assist was first used in 1959 when the Soviet probe "Luna 3" photographed the far side of earth's moon. The maneuver relied on research performed at the Department of Applied Mathematics of Steklov Institute. [ru icon [http://www.applmat.ru/pages/anniver/achievment/3_appl_mech.htm 50th anniversary of Institute for Applied Mathematics - Applied celestial mechanics] - at the website of
Keldysh Institute of Applied Mathematics] [Egorov, Vsevolod Alexandrovich (1957) “Specific problems of a flight to the moon,” "Physics - Uspekhi", Vol. 63, No. 1a, pages 73-117.
Egorov’s work is mentioned in: Boris V. Rauschenbakh, Michael Yu. Ovchinnikov, and Susan M. P. McKenna-Lawlor, "Essential Spaceflight Dynamics and Magnetospherics" (Dordrecht, Netherlands: Kluwer Academic Publishers, 2002), pages 146-147. (The latter reference is available on-line at: http://books.google.com/books?id=m22bjIWZU9MC&pg=PA146&lpg=PA146&dq=institute+applied+mathematics+moscow+%22gravity+assist%22&source=web&ots=U-tZaqVFhE&sig=LT_eEZcCegkd1dDS79glEkT28sw&hl=en#PPA146,M1 .)]
A slingshot maneuver around a planet changes a spacecraft's
velocityrelative to the Sun, even though it preserves the spacecraft's speedrelative to the planet—as it must according to the law of conservation of energy. To a first approximation, from a large distance, the spacecraft appears to have bounced off the planet. Physicists call this an elastic collisioneven though no contact actually occurs.
Why gravitational slingshots are used
A spacecraft traveling to an inner planet will accelerate because it is falling toward the Sun, and a spacecraft traveling to an outer planet will decelerate because it is leaving the vicinity of the Sun.
Although it is true that the orbital speed of an inner planet is greater than that of the Earth, a spacecraft traveling to an inner planet is accelerated by the Sun's gravity to a speed notably greater than the orbital speed of that destination planet. If the spacecraft's purpose is only to fly by the inner planet, then there is typically no need to slow the spacecraft. However, if the spacecraft is to be inserted into
orbitabout that inner planet, then there must be a mechanism to slow the spacecraft.
Likewise, although it is true that the orbital speed of an outer planet is less than that of the Earth, a spacecraft traveling to an outer planet is decelerated by the Sun's gravity to a speed far less than the orbital speed of that outer planet. Thus there must be a mechanism to accelerate the spacecraft. Also, accelerating the spacecraft will, of course, reduce the travel time.
Rocket engines can certainly be used to accelerate and decelerate the spacecraft. However, rocket thrust takes fuel, fuel has mass, and even a small amount of additional mass requirement in the interplanetary vehicle translates to considerably larger engines for raising the spacecraft from the Earth. This is because not only must the primary engines lift that additional mass out of the Earth's gravity well, they must now lift the additional mass of the extra fuel used to lift that additional mass. Thus the liftoff mass requirement increases (roughly) exponentially with an increase in the mass requirement of the payload.
With gravity assist, a spacecraft can be accelerated or decelerated without the need for additional fuel. Also,
aerobrakingcan be used for deceleration, when convenient. The combination of gravity assist and aerobraking, where possible, can save considerable fuel.
As an example, the
MESSENGERmission uses gravity assist to slow the spacecraft on its way to Mercury, but aerobraking cannot be used for insertion into orbit about Mercury because Mercury has almost no atmosphere.
Journeys to the nearest planets,
Marsand Venus, use a Hohmann transfer orbit, an elliptical path which starts as a tangentto one planet's orbit round the sun and finishes as a tangent to the other. This method uses very nearly the smallest possible amount of fuel, but is very slow — it can take over a year to travel from Earth to Mars (fuzzy orbits use even less fuel, but are even slower).
Similarly it might take decades for a spaceship to travel to the outer planets (
Jupiter, Saturn, Uranus, etc.) using a Hohmann transfer orbit, and it would still require far too much fuel, because the spaceship would have to travel for 500 million miles (800 million km) or more against the force of the sun's gravity. Gravitational slingshots offer a way to gain speed without using any fuel, and all missions to the outer planets have used it.Fact|date=January 2008
Limits to slingshot use
The main practical limit to the use of a slingshot is that planets and other large masses are not always in the right places to help a voyage to a particular destination. For example the Voyager missions which started in the late 1970s were made possible by the "Grand Tour" alignment of Jupiter, Saturn, Uranus and Neptune. A similar alignment will not occur again until the middle of the 22nd century. That is an extreme case, but even for less ambitious missions there are years when the planets are not in places that make slingshots useful.
Another limit is caused by the atmosphere of the available planet. The closer the craft can get, the more boost it gets, because gravity falls with the square of distance. If a craft gets too far into the atmosphere, however, the energy lost to friction can exceed that gained from the planet. On the other hand, this effect can be useful if the goal is to lose energy. "See"
Interplanetary slingshots using the sun itself are impossible because the Sun is at rest relative to the solar system as a whole. However, thrusting when near the Sun has the same effect as the powered slingshot described below. This has the potential to magnify a spacecraft's thrusting power enormously, but is limited by the spacecraft's ability to resist the heat.
An "interstellar" slingshot using the Sun is conceivable, involving for example an object coming from elsewhere in our galaxy and slingshotting around the Sun to boost its galactic travel. The energy and angular momentum would then come from the Sun's orbit around the
Milky Way. The time scales involved for such an operation are considerably beyond current human capabilities, however.
Another theoretical limit is based on
general relativity. If a spacecraft gets close to the Schwarzschild radiusof a black hole(the ultimate gravity well), space becomes so curved that slingshot orbits require more energy to escape than the energy that could be added by the black hole's motion.
rotating black holemight provide additional assistance, if its spin axis points the right way. General relativitypredicts that a large spinning mass produces frame-dragging— close to the object, space itself is dragged around in the direction of the spin. In theory an ordinary star produces this effect, although attempts to measure it around the sun have produced no clear results. General relativity predicts that a spinning black hole is surrounded by a region of space, called the ergosphere, within which standing still (with respect to the black hole's spin) is impossible, because space itself is dragged at the speed of light in the same direction as the black hole's spin. The Penrose processmay offer a way to gain energy from the ergosphere, although it would require the spaceship to dump some "ballast" into the black hole, and the spaceship would have had to expend energy to carry the "ballast" to the black hole.
Timeline of notable examples
Mariner 10 – first use
Mariner 10probe was the first spacecraft to use the gravitational slingshot effect to reach another planet, passing by Venus on February 5 1974, on its way to becoming the first spacecraft to explore Mercury.
Voyager 1 – furthest human-made object
July 6, 2007, Voyager 1is over 15.44 terameters (15.44e|12 meters, or 15.44e|9 km, 103.2 AU, or 9.6 billion miles) from the Sun, and is in the boundary zone between the solar system and interstellar space. It gained the energy to escape the sun's gravity completely by performing slingshot maneuvers around Jupiter and Saturn. [ [http://saturn.jpl.nasa.gov/mission/gravity-assist-primer.cfm Cassini-Huygens: Operations - Gravity Assists] ]
Galileo – a change of plan
The Galileo spacecraft was launched by
NASAin 1989 aboard Space Shuttle "Atlantis". Its original mission was designed to use a direct Hohmann transfer, but following the loss of Space Shuttle "Challenger" Galileo's intended Centaur booster rocket was no longer allowed to fly on Shuttles. Using a less-powerful solid booster rocket instead, Galileo flew by Venus once and Earth twice in order to reach Jupiter in December, 1995.
The Galileo engineering inquest speculated (but was never able to conclusively prove) that this longer flight time coupled with the heat near Venus, is what caused lubricant in Galileo's main antenna to fail. This mechanical failure forced the use of a much less powerful backup antenna.
Its subsequent tour of the Jovian moons also used numerous slingshot maneuvers with those moons to conserve fuel and maximize the number of encounters.
The Ulysses probe changed the angle of its trajectory
In 1990, the ESA launched the spacecraft Ulysses to study the polar regions of the
Sun. All the planets orbit approximately in a plane aligned with the equator of the Sun. To move to an orbit passing over the poles of the Sun, the spacecraft would have to eliminate the 30 km/s speed it inherited from the Earth's orbit round the sun and gain the speed needed to orbit the sun in the pole-to-pole plane — tasks which were impossible with current spacecraft propulsionsystems.
The craft was sent towards Jupiter, aimed to arrive at a point in space just "in front of" and "below" the planet. As it passed Jupiter, the probe 'fell' through the planet's gravity field, borrowing a minute amount of momentum from the planet; after it had passed Jupiter, the velocity change had bent the probe's trajectory up out of the plane of the planetary orbits, placing it in an orbit that passed over the poles of the Sun. This maneuver required only enough fuel to send Ulysses to a point near Jupiter, which is well within current technologies.
MESSENGERmission is making extensive use of gravity assists to slow its speed before orbiting Mercury. The MESSENGER mission includesone flyby of Earth, two flybys of Venus, and three flybys of Mercury before finally arriving at Mercury in March 2011 with a velocity low enough to permit orbit insertion with the available fuel. Although the flybys are primarily orbital maneuvers, each provides an opportunity for significant scientific observations.
The Cassini probe – multiple gravity assists
Cassini probepassed by Venus twice, then Earth, and finally Jupiter on the way to Saturn. The 6.7-year transit was slightly longer than the six years needed for a Hohmann transfer, but cut the total amount of delta Vneeded to about 2 km/s, so that the large and heavy Cassini probe was able to reach Saturn even with the small boosters available. A Hohmanntransfer to Saturn would require a total of 15.7 km/s delta V (disregarding Earth's and Saturn's own gravity wells, and disregarding aerobraking), which is not within the capabilities of our current spacecraft boosters.
Suppose that you are a "stationary" observer and that you see: a planet moving left at speed "U"; a spaceship moving right at speed "v". If the spaceship is on the right path, it will pass close to the planet, moving at speed "U + v" relative to the planet's surface because the planet is moving in the opposite direction at speed "U". When the spaceship leaves orbit, it is still moving at "U + v" relative to the planet's surface but in the opposite direction, to the left; and since the planet is moving left at speed "U", the spaceship is moving left at speed "2U + v" from your point of view – its speed has increased by "2U", twice the speed at which the planet is moving.
It might seem that this is oversimplified since we have not covered the details of the orbit, but it turns out that if the spaceship travels in a path which forms a
hyperbola, it can leave the planet in the opposite direction without firing its engine, the speed gain at large distance is indeed "2U" once it has left the gravity of the planet far behind.
This explanation might seem to violate the conservation of energy and momentum, but we have neglected the spacecraft's effects on the planet. The linear momentum gained by the spaceship is equal in magnitude to that lost by the planet, though the planet's large mass makes the resulting change in speed negligibly small. These effects on the planet are so slight (because planets are so much more massive than spacecraft) that they can be ignored in the calculation. [ [http://www.dur.ac.uk/bob.johnson/SL/ The Slingshot Effect] , Durham University]
Realistic portrayals of encounters in space require the consideration of two dimensions. In that case the same principles apply, only adding the planet's velocity requires
vector addition, as shown below.
Gravitational slingshots can also be used to "decelerate" a spacecraft.
Mariner 10did it in 1974 and MESSENGERis also doing it, both to reach Mercury.
If even more speed is needed, the most economical way is to fire a rocket engine near the
periapsis(closest approach). A given rocket burn always provides the same change in velocity ( delta-v), but the change in kinetic energy is proportional to the vehicle's velocity at the time of the burn. So to get the most kinetic energy from the burn, the burn must occur at the vehicle's maximum velocity, at periapsis. Powered slingshots describes this technique in more detail.
A well-established way to get more energy from a gravity assist is to fire a rocket engine at
periapsiswhere a spacecraft is at its maximum velocity.
Rocket engines produce the same force regardless of their velocity. A rocket acting on a fixed object, as in a static firing, does no useful work at all; the rocket's stored energy is entirely expended on its propellant. But when the rocket and payload move, the force applied to the payload by the rocket during any time interval acts through the distance the rocket and payload move during that time. Force acting through a distance is the definition of mechanical energy or work. So the farther the rocket and payload move during any given interval, i.e., the faster they move, the greater the kinetic energy imparted to the payload by the rocket. (This is why rockets are seldom used on slow-moving vehicles; they're simply too inefficient.)
Energy is still conserved, however. The additional energy imparted to the payload is exactly matched by a decrease in energy imparted to the propellant being expelled behind the rocket because the speed of the rocket subtracts from the propellant exhaust velocity. But we don't care about the propellant, so the faster we can move during a rocket burn, the better.
So if we want to impart the maximum amount of
kinetic energyto a spacecraft whose velocity varies with time, we should do it when it's moving the fastest. During a gravity assist, this happens at periapsis, the closest approach to the planet, so that's when we do the burn.
Another way to look at it is that by bringing in propellant as we fell into the planet's gravity well and leaving it there before we climb back out, we are able to extract much of the potential energy that was contained in that propellant.
In popular culture
*The American spacecraft "
Discovery One" uses a gravitational slingshot around Jupiterin Arthur C. Clarke's novel "". The same technique is seen in use in the succeeding novels and .
*The alien ship in
Arthur C. Clarke's novel " Rendezvous with Rama" uses a gravitational slingshot around the Sun.
Heinlein's book The Rolling Stones (novel), there's a description of a powered slingshort around the Earth in the trip from the Moon to Mars.
time travelis achieved by a powered slingshot around the Sun. In the ' episode, " Tomorrow Is Yesterday", a slingshot around the Sun is used to return from the 20th century to the 23rd century (a more plausible result under General Relativity).
*In the "
Star Control" series of games, "gravity whips" are common tactics to employ in order to increase a starship's velocity beyond its normal capacity.
*In the movie "Armageddon", the two space shuttles carrying the drilling crews use a powered slingshot around the moon to intercept the killer
*In the movie "Sunshine", the Icarus II spacecraft uses a slingshot around Mercury to approach the sun.
*In Vernor Vinge's book "
The Peace War", a character wins a video game by using a slingshot maneuver.
*In an episode of the animated television series "
Futurama", Professor Farnsworthuses the principles of slingshot physics to guide a massive garbage ball through space in order to collide with a pre-existing garbage ball so that it might impact the Sun and not the Earth.
*In the pilot of the science-fiction series "
Farscape", astronaut John Crichton is attempting a powered slingshot around Earth when he encounters a wormhole that throws him to the far side of the galaxy. Later in the episode he successfully uses the technique to escape the main antagonist.
*In , the ship with the kids does a powered slingshot around Jupiter.
3753 Cruithne: an asteroid which periodically has gravitational slingshot encounters with Earth.
Flyby anomaly: an anomalous delta-v increase during gravity assists
Oberth effect: doing burns deep in gravity fields gain speed
New Horizons: a gravity-assisted mission (flying past Jupiter) to reach Plutoin 2015.
STEREO: a gravity-assisted mission which used Earth's Moon to eject two spacecraft from Earth's orbit into heliocentricorbit
Interplanetary Transport Network
* [http://www.dur.ac.uk/bob.johnson/SL/ Slingshot effect]
* [http://www.esa.int/esaCP/SEMXLE0P4HD_index_0.html Animation of Cassini Huygens gravitational sling shot]
* [http://www.mathpages.com/home/kmath114.htm MathPages - Gravitational Slingshot Theory]
* [http://saturn.jpl.nasa.gov/mission/gravity-assist-primer.cfm A Quick Gravity Assist Primer]
* [http://solar.cranf.net An artistical simulation of an unstable planetary system showing gravitational slingshots and other phenomena]
* [http://www.jaqar.com Tools to calculate effects of a swing-by, such as the Swing-by Calculator]
Wikimedia Foundation. 2010.
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