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The interplanetary transport network provides low-energy gravitational pathways through the solar system
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Retrieved reference materials and technical discussions confirm that the Interplanetary Transport Network consists of low-energy gravitational pathways utilizing invariant manifolds and Lagrange points to navigate through the solar system.

Evidence for · 4
2020 · cited by 13
Abstract Fast development of CubeSat technology now enables the first interplanetary missions. The potential application of CubeSats to flyby near-Earth asteroids is explored in this paper in consideration of CubeSats' limited propulsive capabilities and systems constraints. Low-energy asteroid flyby trajectories are designed assuming a CubeSat is initially parked around to the Sun-Earth Lagrange points. High-impulse and low-thrust trajectories with realistic thrusting models are computed first in the Circular Restricted Three-Body Problem (CR3BP), and then in a high-fidelity ephemeris model. Analysis in the ephemeris model is used to confirm that trajectories computed in the CR3BP model also exist in a more realistic dynamical model, and to verify the validity of the results obtained in CR3BP analysis. A catalogue of asteroid flyby opportunities between years 2019 and 2030 is provided, with 80 m/s of available ΔV and departure from halo orbits around the first and second Sun-Earth Lagrange points (of similar size to those typically used by scientific missions). Results show that the CR3BP model can serve as an effective tool to identify reachable asteroids and can provide an initial estimation of the ΔV cost in the ephemeris model (with ±15 m/s accuracy). An impulsive maneuver model can also provide an accurate estimation of the ΔV requirement for a CubeSat equipped with a high-impulse thruster (with 4 m/s accuracy), even if its thrust magnitude is small and requires duty cycling; low-thrust ΔV requirements, however, may differ significantly from the impulsive results (±15 m/s). Fitxers 701411.pdf (2.37 MB) Tipus de document Article Versió Versió acceptada Data de publicació 2020 Llicència de publicació Si us plau utilitzeu sempre aquest identificador per citar o enllaçar aquest document: https://hdl.handle.net/2445/194753 High-fidelity trajectory design to flyby near-earth asteroids using cubesats Títol de la revista Autors Machuca, P. Sánchez, J.P. Masdemont, Josep J. Gómez Muntané, Gerardo Director/Tutor ISSN de la revista Títol del volum Recurs relacionat https://doi.org/10.1016/j.actaastro.2019.09.041 Resum Fast development of CubeSat technology now enables the first interplanetary missions. The potential application of CubeSats to flyby near-Earth asteroids is explored in this paper in consideration of CubeSats' limited pro- pulsive capabilities and systems constraints. Low-energy asteroid flyby trajectories are designed assuming a CubeSat is initially parked around to the Sun-Earth Lagrange points. High-impulse and low-thrust trajectories with realistic thrusting models are computed first in the Circular Restricted Three-Body Problem (CR3BP), and then in a high-fidelity ephemeris model. Analysis in the ephemeris model is used to confirm that trajectories computed in the CR3BP model also exist in a more realistic dynamical model, and to verify the validity of the results obtained in CR3BP analysis. A catalogue of asteroid flyby opportunities between years 2019 and 2030 is provided, with 80 m/s of availableΔV and departure from halo orbits around the first and second Sun-Earth Lagrange points (of similar size to those typically used by scientific missions). Results show that the CR3BP model can serve as an effective tool to identify reachable asteroids and can provide an initial estimation of the ΔV cost in the ephemeris model (with ± 15 m/s accuracy). An impulsive maneuver model can also provide an accurate estimation of theΔV requirement for a CubeSat equipped with a high-impulse thruster (with 4 m/s accuracy), even if its thrust magnitude is small and requires duty cycling; low-thrustΔV requirements, however, may differ significantly from the impulsive results ( ± 15 m/s). Més... Matèries Satèl·lits artificials , Dinàmica Matèries (anglès) Artificial satellites , Dynamics Citació Col·leccions Articles publicats en revistes (Matemàtiques i Informàtica) Pàgina completa de l'ítem Citació ISO 690 APA MLA Chicago/Turabian Vancouver IEEE BibTeX RIS MACHUCA, P., et al.
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region and transporting them elsewhere in the Solar System, perhaps via the proposed Interplanetary Transport Network, may be feasible in the not-so-distant Space colonization, or extraterrestrial colonization, is the establishment of human settlements or colonies in outer space and on astronomical bodies. The concept, in its broadest sense, has been applied to any permanent human presence in space, such as a space habitat or other extraterrestrial settlements. It may involve notions of territorial occupation, resource control for economic or military The Moon is discussed as a target for colonization, due to its proximity to Earth and lower escape velocity. The Moon is reachable from Earth in three days, has a near-instant communication to Earth, with minable minerals, no atmosphere, and low gravity, making it extremely easy to ship materials and products to orbit. Abundant ice is trapped in permanently shadowed craters near the poles, which could provide support for the water needs of a lunar colony, though indications that mercury is also similarly trapped there may pose health concerns. Native precious metals, such as gold, silver, and probably platinum, are also concentrated at the lunar poles by electrostatic dust transport. There are only a few materials on the Moon which have been identified to make economic sense to ship directly back to the Earth, which are helium-3 (for fusion power) and rare-earth minerals (for electronics). Instead, it makes more sense for these materials to be used in-space or being turned into valuable products for export. However, the Moon's lack of atmosphere provides no protection from space radiation or meteoroids, so lunar lava tubes have been proposed sites to gain protection. The Moon's low surface gravity is also a concern, as it is unknown whether 1/6g is enough to maintain human health for long periods. Since the Moon has extreme… Th… Ganymede is the largest moon in the Solar System. Ganymede is the only moon with a magn Use of geothermal systems to generate power may be practical on some of the planets and moons of the solar system. === This can lead to exhaustion, as well as other sleep problems such as insomnia, which can reduce their productivity and lead to mental health disorders. High-energy radiation is a health risk that colonists would face, as radiation in deep space is deadlier than what astronauts face now in low Earth orbit. Metal shielding on space vehicles protects against only 25–30% of space radiation, possibly leaving colonists exposed to the other 70% of radiation and its short and long-term health complications. == Locations == Space colonization has been envisioned at many different locations inside and outside the Solar System, but most commonly at Mars and the Moon. If Martian materials can be used to make propellant (such as methane with the Sabatier process) and supplies (such as oxygen for crews), the amount of supplies needed to bring to Mars can be greatly reduced. Even then, Mars colonies will not be economically viable in the near term; thus, reasons for colonizing Mars will be mostly ideological and prestige-based, such as a desire for freedom. === Other inner Solar System bodies === ==== Mercury ==== Mercury is rich in metals and volatiles, as well as solar energy. However, Mercury is the most energy-consuming body on the Solar System to land for spacecraft launching from Earth, and astronauts there must contend with the extreme temperature differential and radiation. Once thought to be a volatile-depleted body like the Moon, Mercury is now known to be volatile-rich, surprisingly richer in volatiles than any other terrestrial body in the inner Solar System. The planet also receives six and a half times the solar flux as the Earth/Moon system, making solar energy an effective energy source; it could be harnessed through orbital solar arrays and beamed to the surface or exported to other planets. Because of this magnetic field, Ganymede is one of only two Jovian moons where surface settlements would be feasible because it receives about 0.08 Sv of radiation per day. Ganymede could be terraformed. The Keck Observatory announced in 2006 that the binary Jupiter trojan 617 Patroclus, and possibly many other Jupiter trojans, are likely composed of water ice, with a layer of dust. This suggests that mining water and other volatiles in this region and transporting them elsewhere in the Solar System, perhaps via the proposed Interplanetary Transport Network, may be feasible in the not-so-distant future. This could make colonization of the Moon, Mercury and main-belt asteroids more practical. An alternative model of Enceladus's activity is the decomposition of methane/water clathrates – a process requiring lower temperatures than liquid water eruptions. The higher density of Enceladus indicates a larger than Saturnian average silicate core that could provide materials for base operations. ===== Titan ===== Authors like Robert Zubrin have offered that Saturn is the most important and valuable of the four gas giants in the Solar System, because of its relative proximity, low radiation, and excellent system of moons. He named Titan as the best candidate on which to establish a base to exploit the resources of the Saturn system. Some estimates suggest that abundant energy resources on Titan could power a colony with a population size of the United States. The dense atmosphere of Titan shields the surface from radiation and would make any structural failures problematic, rather than catastrophic. With an oxygen mask and thermal clothing protection, humans could roam Titan's surface in the dim sunlight. Or, given the low gravity and dense atmosphere, they could float above it in a balloon or on personal wings. === Trans-Neptunian region === === Beyond the Solar System === Beyond the Solar System colonization targets might be identified in the surrounding stars. The main difficulty is the vast distances to other stars.
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than those of the Interplanetary Transport Network, but the reduction in transfer time comes at the cost of increased Δv requirements. The Easily Recoverable Asteroid mining is the hypothetical and technically possible extraction of materials from asteroids and other minor planets, including near-Earth objects. Research missions focused on asteroid sample return, including Hayabusa, Hayabusa2, OSIRIS-REx, and Tianwen-2, illustrate the challenges of collecting ore from space using current technology. As of 2024, around 127 grams of asteroid material hav As… As concerns about resource depletion on Earth have increased, the prospect of extracting valuable elements from asteroids for use on Earth—or using space-based resources to build solar-power satellites and space habitats, has attracted greater interest. Hypothetically, water processed from ice could refuel orbiting propellant depots. Although asteroids and Earth accreted from the same starting materials, Earth's relatively stronger gravity pulled all heavy siderophilic (iron-loving) elements into its core during its molten youth more than four billion years ago. This left the crust depleted of such valuable elements until a rain of asteroid impacts re-infused the depleted crust with metals like gold, cobalt, iron, manganese, molybdenum, nickel, osmium, palladium, platinum, rhenium, rhodium, ruthenium and tungsten (some flow from core to surface does occur, e.g. at the Bushveld Igneous Complex, a famously rich source of platinum-group metals). Today, these metals are mined from Earth's crust, and they are essential for economic and technological progress. Hence, the geologic history of Earth may have set the stage for a future of asteroid mining. In 2006, the Keck Observatory announced that the binary Jupiter trojan 617 Patroclus, and possibly large numbers of other Jupiter trojans, are likely extinct comets and consist largely of water ice. Similarly, Jupiter-family comets, and possibly near-Earth asteroids that are extinct comets, might also provide water. The process of in-situ resource utilization—using materials native to space for propellant, thermal management, tankage, radiation shielding, and other high-mass components of space infrastructure—could lead to radical reductions in its cost. Although whether these cost reductions could be achieved, and if achieved would offset the enormous infrastructure investment required, is unclear. From the astrobiological perspective, asteroid prospecting could provide scientific data for the search for extraterrestrial intelligence (SETI). Some astrophysicists have suggested that if advanced extraterrestrial civilizations employed asteroid mining long ago, the hallmarks of these activities might be detectable. An important factor to consider in target selection is orbital economics, in particular the change in velocity (Δv) and travel time to and from the target. More of the extracted native material must be expended as propellant in higher Δv trajectories, thus less would be returned as payload. Direct Hohmann trajectories are faster than Hohmann trajectories assisted by planetary and/or lunar flybys, which in turn are faster than those of the Interplanetary Transport Network, but the reduction in transfer time comes at the cost of increased Δv requirements. In-space manufacturing (ISM), which may be enabled by biomining. Bring raw asteroidal material to Earth for use. Process asteroidal material on-site to bring back only processed materials, and perhaps produce propellant for the return trip. Transport the asteroid to a safe orbit around the Moon or Earth or to a space station. This can hypothetically allow for most materials to be used and not wasted. Processing in situ for the purpose of extracting high-value minerals will reduce the energy requirements for transporting the materials, although the processing facilities must first be transported to the mining site. In situ mining will involve drilling boreholes and injecting hot fluid/gas and allow the useful material to react or melt with the solvent and extract the solute. Due to the weak gravitational fields of asteroids, any activities, like drilling, will cause large disturbances and form dust clouds. These might be confined by some dome or bubble barrier. Or else some means of dissipating any dust could be provided. Mining operations require special equipment to handle the extraction and processing of ore in outer space. The machinery will need to be anchored to the body, but once in place, the ore can be moved about more readily due to the lack of gravity. However, no techniques for refining ore in zero gravity currently exist. Docking with an asteroid might be performed using a harpoon-like process, where a projectile would penetrate the surface to serve as an anchor; then an attached cable would be used to winch the vehicle to the surface, if the asteroid is both penetrable and rigid enough for a harpoon to be effective. Due to the distance from Earth to an asteroid selected for mining, the round-trip time for communications will be several minutes or more, except during occasional close approaches to Earth by near-Earth asteroids. Thus any mining equipment will either need to be highly automated, or a human presence will be needed nearby. Humans would also be useful for troubleshooting problems and for maintaining the equipment. On the other hand, multi-minute communications delays have not prevented the success of robotic exploration of Mars, and automated systems would be much less expensive to build and deploy. Research and development costs Exploration and prospecting costs Construction and infrastructure development costs Operational and engineering costs Environmental costs Time cost Determining financial feasibility is best represented through net present value. One requirement needed for financial feasibility is a high return on investment estimating around 30%. Example calculation assumes for simplicity that the
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# How are Interplanetary Transport Network/Weak Stability Boundary paths calculated? Tags: interplanetary, delta-v, low-energy-transfer - Score: 3 - Views: 480 - Answers: 2 - Answered: yes - Asked by: hi-bye125 (442 rep) - Asked: 2023-12-27 - Edited: 2023-12-29 - Site: space ## Question While reading up a bit online, I found out about Weak Stability Boundaries and the Interplanetary transport network. How is this "path" that traverses the Solar System determined? I am aware of some relation to Lambert's problem, but am only familiar with the 2 body form of this. ITN for reference below: ## Answers ### Answer by Woody (score: 4) Mathspeak answer: The pathways of the Interplanetary Transportation Network (ITN) are determined using numerical analysis of a dynamical system of equations of motion to find invariant manifolds which allow low-energy trajectories between Lagrange points of different celestial bodies. What on Earth does all that mean? Numerical analysis means you use lots of arithmetic to get an approximate solution to a problem you don’t know how to solve exactly. For instance, say you want to know the area of a circular courtyard. A “numerical solution” is to lay do
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This check searched the claim as stated. It did not run a separate search for evidence against it.
  1. Space colonizationreferencesame source L1no side taken
  2. High-fidelity trajectory design to flyby near-Earth asteroids using CubeSatspeer-reviewedno side taken
  3. Asteroid miningreferencesame source L1no side taken
  4. How are Interplanetary Transport Network/Weak Stability Boundary paths calculated?referenceno side taken
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