Interplanetary Transport Network

Source: Wikipedia, the free encyclopedia.
Not to be confused with
Interplanetary Transport System
.
Lagrange points, while constricted areas represent locations where objects linger in temporary orbit
around a point before continuing on.

The Interplanetary Transport Network (ITN)

trajectories through space can be redirected using little or no energy. These points have the peculiar property of allowing objects to orbit around them, despite lacking an object to orbit[further explanation needed]. While it would use little energy, transport along the network would take a long time.[2]

History

Interplanetary transfer orbits are solutions to the gravitational three-body problem, which, for the general case, does not have analytical solutions, and is addressed by numerical analysis approximations. However, a small number of exact solutions exist, most notably the five orbits referred to as "Lagrange points", which are orbital solutions for circular orbits in the case when one body is significantly more massive.

The key to discovering the Interplanetary Transport Network was the investigation of the nature of the winding paths near the Earth-Sun and Earth-Moon Lagrange points. They were first investigated by Henri Poincaré in the 1890s. He noticed that the paths leading to and from any of those points would almost always settle, for a time, on an orbit about that point.[3] There are in fact an infinite number of paths taking one to the point and away from it, and all of which require nearly zero change in energy to reach. When plotted, they form a tube with the orbit about the Lagrange point at one end.

The derivation of these paths traces back to mathematicians Charles C. Conley and Richard P. McGehee in 1968.[4] Hiten, Japan's first lunar probe, was moved into lunar orbit using similar insight into the nature of paths between the Earth and the Moon. Beginning in 1997, Martin Lo, Shane D. Ross, and others wrote a series of papers identifying the mathematical basis that applied the technique to the Genesis solar wind sample return, and to lunar and Jovian missions. They referred to it as an Interplanetary Superhighway (IPS).[5]

Paths

As it turns out, it is very easy to transit from a path leading to the point to one leading back out. This makes sense, since the orbit is unstable, which implies one will eventually end up on one of the outbound paths after spending no energy at all.

weak stability boundary"[6] or "fuzzy boundary"[7]
for this effect.

With careful calculation, one can pick which outbound path one wants. This turns out to be useful, as many of these paths lead to some interesting points in space, such as the Earth's Moon or between the Galilean moons of Jupiter, within a few months or years.[8]

For trips from Earth to other planets, they are not useful for crewed or uncrewed probes, as the trip would take many generations. Nevertheless, they have already been used to transfer spacecraft to the Earth–Sun L1 point, a useful point for studying the Sun that was employed in a number of recent missions, including the Genesis mission, the first to return solar wind samples to Earth.[9] The network is also relevant to understanding Solar System dynamics;[10][11] Comet Shoemaker–Levy 9 followed such a trajectory on its collision path with Jupiter.[12][13]

Further explanation

The ITN is based around a series of orbital paths predicted by

restricted three-body problem leading to and from the orbits around the Lagrange points – points in space where the gravity between various bodies balances with the centrifugal force of an object there. For any two bodies in which one body orbits around the other, such as a star/planet or planet/moon system, there are five such points, denoted L1 through L5. For instance, the Earth–Moon L1 point lies on a line between the two, where gravitational forces between them exactly balance with the centrifugal force of an object placed in orbit there. These five points have particularly low delta-v requirements, and appear to be the lowest-energy transfers possible, even lower than the common Hohmann transfer orbit
that has dominated orbital navigation since the start of space travel.

Although the forces balance at these points, the first three points (the ones on the line between a certain large mass, e.g. a star, and a smaller, orbiting mass, e.g. a planet) are not stable equilibrium points. If a spacecraft placed at the Earth–Moon L1 point is given even a slight nudge away from the equilibrium point, the spacecraft's trajectory will diverge away from the L1 point. The entire system is in motion, so the spacecraft will not actually hit the Moon, but will travel in a winding path, off into space. There is, however, a semi-stable orbit around each of these points, called a halo orbit. The orbits for two of the points, L4 and L5, are stable, but the halo orbits for L1 through L3 are stable only on the order of months.

In addition to orbits around Lagrange points, the rich dynamics that arise from the gravitational pull of more than one mass yield interesting trajectories, also known as

low energy transfers.[4] For example, the gravity environment of the Sun–Earth–Moon system allows spacecraft to travel great distances on very little fuel,[citation needed
] albeit on an often circuitous route.

Missions

Launched in 1978, the

geomagnetic tail and a comet flyby. The mission was subsequently renamed the International Cometary Explorer
(ICE).

The first low energy transfer using what would later be called the ITN was the rescue of Japan's Hiten lunar mission in 1991.[15]

Another example of the use of the ITN was NASA's 2001–2003 Genesis mission, which orbited the Sun–Earth L1 point for over two years collecting material, before being redirected to the L2 Lagrange point, and finally redirected from there back to Earth.[1]

The 2003–2006 SMART-1 of the European Space Agency used another low energy transfer from the ITN.[citation needed]

In a more recent example, the

Chinese spacecraft Chang'e 2 used the ITN to travel from lunar orbit to the Earth-Sun L2 point, then on to fly by the asteroid 4179 Toutatis.[citation needed
]

Asteroids

The asteroid 39P/Oterma's path from outside Jupiter's orbit, to inside, and back to outside is said to follow these low energy paths.[1]

See also

References

  1. ^
    doi:10.1511/2006.59.994. Archived
    (PDF) from the original on 2013-10-20. Retrieved 2013-06-27.
  2. ^ "The Interplanetary Superhighway; Shane Ross; Virginia Tech". Archived from the original on 2019-06-15. Retrieved 2016-12-30.
  3. doi:10.1090/S0273-0979-05-01085-2
    .
  4. ^
    JSTOR 2099124
    .
  5. ^ Lo, Martin W. and Ross, Shane D. (2001) The Lunar L1 Gateway: Portal to the Stars and Beyond Archived 2013-01-15 at the Wayback Machine, AIAA Space 2001 Conference, Albuquerque, New Mexico.
  6. ^ Edward A. Belbruno; John P. Carrico (2000). "Calculation of Weak Stability Boundary Ballistic Lunar Transfer Trajectories" (PDF). AIAA/AAS Astrodynamics Specialist Conference. Archived (PDF) from the original on 2008-11-20. Retrieved 2017-08-29.
  7. ^ Frank, Adam (September 1994). "Gravity's Rim". Discover. Archived from the original on 22 October 2019. Retrieved 29 August 2017.
  8. ^ Ross, S.D., W.S. Koon, M.W. Lo and J.E. Marsden (2003) Design of a Multi-Moon Orbiter Archived 2007-01-08 at the Wayback Machine. 13th AAS/AIAA Space Flight Mechanics Meeting, Ponce, Puerto Rico, Paper No. AAS 03–143.
  9. ^ Lo, M. W., et al. 2001. Genesis Mission Design, The Journal of the Astronautical Sciences 49:169–184.
  10. ^ Belbruno, E., and B.G. Marsden. 1997. Resonance Hopping in Comets. The Astronomical Journal 113:1433–1444
  11. PMID 12779398. Archived
    (PDF) from the original on 2018-07-19. Retrieved 2019-09-23.
  12. ^ Smith, D. L. 2002. Next Exit 0.5 Million Kilometers Archived 2003-03-29 at the Wayback Machine. Engineering and Science LXV(4):6–15
  13. ^ Ross, S. D. 2003. Statistical theory of interior–exterior transition and collision probabilities for minor bodies in the solar system Archived 2007-01-08 at the Wayback Machine, Libration Point Orbits and Applications (Eds. G Gomez, M.W. Lo and J.J. Masdemont), World Scientific, pp. 637–652.
  14. doi:10.2514/3.56034
    .
  15. ISBN 9780691094809. Archived from the original
    on 2014-12-02. Retrieved 2006-09-25.

Further reading

External links

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