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Questions tagged [low-energy-transfer]

Questions on trajectories that allow spacecraft to change orbits using very little fuel.

1 vote
0 answers
88 views

Cyclers work by taking advantage of alignments in planets' orbits, but since coincidental "resonances" do have slight variations, they require regular corrections; how would you calculate ...
avivtheprogrammer's user avatar
2 votes
1 answer
122 views

The Apollo lunar missions used a free return trajectory which resembles a figure-8 when plotted in an Earth/Moon rotating frame of reference. This trajectory was chosen for safety: if the mission was ...
Woody's user avatar
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3 votes
0 answers
79 views

I am familiar with computing rendezvous maneuvers using a Hohmann transfer when the two orbits are circular. However, when both orbits are highly elliptical, the fairly simple calculations with a ...
Leonard's user avatar
  • 59
9 votes
2 answers
1k views

I know that a Mars Cycler has many advantages due to the distance involved, but what about a Lunar Cycler? From what I've seen, the time window seems relatively short, and docking with a cycler ...
Just passing by's user avatar
3 votes
2 answers
381 views

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 ...
hi-bye125's user avatar
  • 442
4 votes
1 answer
239 views

My nomenclature might be a bit off, I’m no expert but I’ve been reading to solve the question all the same. Say we detect an orbit transfer based off ephemeris records. We can get the 6 classic orbit ...
Dylan's user avatar
  • 331
7 votes
2 answers
2k views

The Philae lander bounced off 67P/C-G due to low gravity, but how high did it actually bounce?
Mar's user avatar
  • 73
5 votes
3 answers
2k views

As a (very late) follow up to this question, I wondered if there are any ITN paths that leave the solar system altogether? Articles about this seem to be concerned with low energy transfers of ...
Dave Gremlin's user avatar
  • 3,405
4 votes
1 answer
292 views

Being a newbie, I humbly submit the following question : How to minimize the energy (in terms of delta-v burns) to transfer a mass of 1 metric ton (1000kg) from Very Low Earth Orbit (say 200km above ...
C. Burns's user avatar
  • 159
5 votes
1 answer
2k views

Imagine arriving at Saturn, jettisoning your passenger cargo, and then utilizing the massive gravitational pull of the gas giant to slingshot back towards Jupiter. Due to the immense mass of these ...
Enoch's user avatar
  • 317
2 votes
0 answers
63 views

In my MSc thesis I faced the problem of unstable hyperbolic invariant manifold trajectories (UHIMs) emanating from planar Lyapunov orbits around two collinear Lagrange points L1 and L2 of the Sun-...
g_don's user avatar
  • 433
5 votes
2 answers
543 views

I decided to fly to Mars in KSP using a slingshot of Venus to see if I could save fuel. Since Venus is closer to Earth, you need less fuel to get there. When I tested it I used less fuel, but the ...
The Rocket fan's user avatar
2 votes
0 answers
156 views

This is part of the code I used, where EM: Earth moon ...
Aabha Awere's user avatar
3 votes
1 answer
189 views

I'm examining entering lunar orbit through the Earth-Moon L1 point with low-thrust propulsion. As part of this, I'm interested in all examples of spacecraft (both actually flown and ones that didn't ...
NeutronStar's user avatar
  • 1,059
6 votes
1 answer
685 views

In 1985 Buzz Aldrin AKA “Dr. Rendezvous” proposed using a pair of space station habitats in solar cycler orbits as “Up and Down Escalators” for crewed Earth-Mars transfers. https://en.wikipedia.org/...
Woody's user avatar
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