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Low-energy transfer

Low-energy transfer is a physics topic covered in the lgStudy science library. This page brings together a partial reference excerpt, illustrations, worked examples, real-world applications and a short study plan, so you can understand Low-energy transfer rather than just read about it. In short: A low-energy transfer, or low-energy trajectory, is a route in space that allows spacecraft to change orbits using significantly less fuel than traditional transfers. These routes work in the Earth–Moon system and also in other systems, such as between the moons of Jupiter.

Low-energy transfer — main illustration
Low-energy transfer — illustration

Key takeaways

  • Low-energy transfer belongs to physics; place it in that map before memorising details.
  • Learn the definition first, then one example that makes the definition concrete.
  • Connect Low-energy transfer to a quantity you can measure, compute or draw — that is where exam questions come from.
  • Reproduce the core statement of Low-energy transfer from memory before moving on to harder problems.

Reference excerpt

A low-energy transfer, or low-energy trajectory, is a route in space that allows spacecraft to change orbits using significantly less fuel than traditional transfers. These routes work in the Earth–Moon system and also in other systems, such as between the moons of Jupiter. The drawback of such trajectories is that they take longer to complete than higher-energy (more-fuel) transfers, such as Hohmann transfer orbits. Low-energy transfers are also known as weak stability boundary trajectories, and include ballistic capture trajectories. Low-energy transfers follow special pathways in space, sometimes referred to as the Interplanetary Transport Network. Following these pathways allows for long distances to be traversed for little change in velocity, or delta-v.

Example missions

Missions that have used low-energy transfers include:

Hiten, from JAXA SMART-1, from ESA Genesis, from NASA. GRAIL, from NASA. Danuri from KARI On-going missions that use low-energy transfers include:

BepiColombo, from ESA/JAXA CAPSTONE from NASA SLIM, from JAXA Proposed missions using low-energy transfers include:

European Student Moon Orbiter (ESMO) Mars Direct

History Low-energy transfers to the Moon were first demonstrated in 1991 by the Japanese spacecraft Hiten, which was designed to swing by the Moon but not to enter orbit. The Hagoromo subsatellite was released by Hiten on its first swing-by and may have successfully entered lunar orbit, but suffered a communications failure. Edward Belbruno and James Miller of the Jet Propulsion Laboratory had heard of the failure, and helped to salvage the mission by developing a ballistic capture trajectory that would enable the main Hiten probe to itself enter lunar orbit. The trajectory they developed for Hiten used Weak Stability Boundary Theory and required only a small perturbation to the elliptical swing-by orbit, sufficiently small to be achievable by the spacecraft's thrusters. This course would result in the probe being captured into temporary lunar orbit using zero delta-v, but required five months instead of the usual three days for a Hohmann transfer.

Delta-v savings From low Earth orbit to lunar orbit, the delta-v savings approach 25% on the burn applied after leaving low Earth orbit, compared to the retrograde burn applied near the Moon in the traditional trans-lunar injection, and allow for a doubling of payload. Robert Farquhar has described a 9-day route from low earth orbit to lunar capture that takes 3.5 km/s. Belbruno's routes from low Earth orbit require a 3.1 km/s burn for trans lunar injection, a delta-v saving of not more than 0.4 km/s. However, the latter require no large delta-v change after leaving low Earth orbit, which may have operational benefits if using an upper stage with limited restart or in-orbit endurance capability, which would require the spacecraft to have a separate main propulsion system for capture. For rendezvous with the Martian moons, the savings are 12% for Phobos and 20% for Deimos. Rendezvous is targeted because the stable pseudo-orbits around the Martian moons do not spend much time within 10 km of the surface.

See also

Bi-elliptic transfer Delta-v budget Gravity assist Interplanetary Transport Network Orbital mechanics

References

External links Celestial Mechanics Theory Meets the Nitty-Gritty of Trajectory Design Earth-to-Moon Low Energy Transfers Targeting L1 Hyperbolic Transit Orbit June 2005 Low Energy Trajectories and Chaos: Applications to Astrodynamics and Dynamical Astronomy Navigating Celestial Currents

Illustrations

Low-energy transfer: An example of Low-energy transfer to the Moon.mw-parser-output .legend{page-break-inside:avoid;break-inside:avoid-column}.mw-parser-output .legend-color{display:inline-block;min-width:1.25em;height:1.25em;line-height:1.25;margin:1px 0;text-align:center;border:1px solid black;background-color:transparent;color:black}.mw-parser-output .legend-text{}   GRAIL-A ·   Moon ·   Earth
An example of Low-energy transfer to the Moon.mw-parser-output .legend{page-break-inside:avoid;break-inside:avoid-column}.mw-parser-output .legend-color{display:inline-block;min-width:1.25em;height:1.25em;line-height:1.25;margin:1px 0;text-align:center;border:1px solid black;background-color:transparent;color:black}.mw-parser-output .legend-text{}   GRAIL-A ·   Moon ·   Earth
Low-energy transfer: SLIM's trajectory included a low energy transfer
SLIM's trajectory included a low energy transfer

Worked examples

Example 1 — a first encounter with Low-energy transfer

Start with the simplest possible case. Write down what Low-energy transfer claims or describes in one sentence, then invent the smallest concrete situation in which that sentence is true. In physics, the smallest case is usually a single object, a single equation or a single measurement. Check that every symbol or term in your sentence has a meaning in that case.

Example 2 — changing one variable

Take the situation from Example 1 and change exactly one quantity: double it, halve it, or set it to zero. Predict what should happen to Low-energy transfer before you calculate. Comparing your prediction with the result is the fastest way to find out whether you understand the idea or only the words.

Example 3 — an exam-style question

Typical questions about Low-energy transfer ask you to (a) state it precisely, (b) apply it to given data, and (c) explain a limitation. Practise writing all three answers in under five minutes; the third part is what separates a full-mark answer from an average one.

Applications of Low-energy transfer

In research
Low-energy transfer appears in physics research whenever the underlying quantities have to be modelled precisely. Papers usually cite it as a starting assumption and then explore where it breaks down.
In technology and industry
Engineering practice reuses Low-energy transfer in design rules, simulations and safety margins. Knowing the idea lets you read a specification sheet and understand why the numbers look the way they do.
In the classroom
Low-energy transfer is common in secondary-school and first-year university syllabi. It links to neighbouring topics Astrodynamics, so understanding it makes those chapters shorter.
In everyday life
Look for Low-energy transfer outside the textbook — in sport, cooking, traffic, electronics or the sky above you. An example you found yourself is remembered far longer than one you were given.
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How to study Low-energy transfer in 20 minutes

  1. Read the reference excerpt below once, without taking notes.
  2. Close the page and write down what Low-energy transfer means in your own words.
  3. Compare your version with the excerpt and mark what you missed.
  4. Work through the three examples above with pen and paper.
  5. Explain Low-energy transfer out loud to somebody else — or to Teacher Smith in the lgStudy chat.

Frequently asked questions

What is Low-energy transfer in simple terms?

A low-energy transfer, or low-energy trajectory, is a route in space that allows spacecraft to change orbits using significantly less fuel than traditional transfers. These routes work in the Earth–Moon system and also in other systems, such as between the moons of Jupiter.

Why does Low-energy transfer matter?

Because it connects several physics ideas at once: it gives you a definition you can apply, a quantity you can calculate, and a way to check whether a result is plausible.

How should I study Low-energy transfer?

Read the excerpt, restate it from memory, then work through the examples and applications listed on this page. The five-step study plan above takes about twenty minutes.

What does this page cover?

It gives you a compact reference excerpt plus original lgStudy explanations, examples, applications and study material on Low-energy transfer.

Tags

  • Astrodynamics

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