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Questions tagged [orbital-maneuver]

In spaceflight, an orbital maneuver is the use of propulsion systems to change the orbit of a spacecraft.

39 questions with no upvoted or accepted answers
6votes
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What is Tiangong-2 doing?

Some news in various outlets following some twitterings including this tweet by Jonathan McDowell about Tiangong-2 performing a sizeable orbit-lowering, followed by a re-raising: ‏ OK now that's ...
uhoh's user avatar
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Why doesn't SpaceX know how long orbital maneuver burns will take?

While listening in on today's Crew Dragon 1 rendezvous, I noticed something interesting: the announced duration for the final coelliptic burn was "25 to 35 seconds". And this wasn't just a ...
Mark's user avatar
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How would I or who/what could help me find the trajectory of an "Extended Grand Tour" spacecraft, without having to take a long course on the subject?

(As forewarning, the most integral details of this question are bolded.) For context, I have been writing an alternate history involving the accelerated development of spaceflight technology for over ...
Grant Hartlage's user avatar
4votes
0answers
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Is there a known solution for optimal impulsive transfer between two arbitrary elliptical orbits?

If not, what optimization methods or tools do people use? (Code libraries?)
3uluner's user avatar
4votes
0answers
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How many burns does it take to reboost the ISS?

When the International Space Station is given a reboost, how many burns are performed? Is it a Hohmann transfer orbit, with one perigee burn and one apogee burn? Or is it one burn at apogee just to ...
DrSheldon's user avatar
4votes
0answers
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How do I calculate the change in the argument of periapsis after a plane change maneuver?

Let's say I have a spacecraft in an initial geocentric orbit with the following parameters: a = 7,960,000 m, e = 0.010, $\Omega$ = 180$^{\circ}$, i = 98$^{\circ}$, $\omega$ = 90$^{\circ}$, $\theta_0$ =...
ReluctantEarthling's user avatar
4votes
0answers
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Proper handling of terminal guidance of finite burn closed-loop execution for rendezvous conditions?

I'm writing some software which uses Optimal Control Theory / Calculus of Variations / Pontrayagin's Minimum Principle / Primer Vector Theory to do closed-loop execution of finite burns (in KSP). ...
lamont's user avatar
3votes
0answers
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Mean motion as indication for satellite (evasion) maneuvers

I am interested in detecting satellite maneuvers, e.g., to avoid collissions. As far as I understand the best publicly available data comes from TLEs although they have their own problems. What is the ...
Adrian's user avatar
3votes
0answers
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Eutelsat 13G and Spacebus NEO's all-electric propulsion

Today, Eutelsat's Hotbird-13G was launched by a Falcon 9 to a "geosynchronous transfer orbit". Deployment was at an altitude of roughly 1100 km. The satellite must reach a geosynchronous ...
Peter - Reinstate Monica's user avatar
3votes
0answers
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What engine burn/thrust could be used for satellite longitudinal change?

If you wish to change the longitude (but not the inclination) of a satellite in Low Earth Orbit, what kind of maneuvers could you use? I am no expert, but let's say ISS or Hubble would like to stop "...
spa's user avatar
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Transfer between circular orbits in up to 5 maneuvers

There are 2 circular orbits with different inclination and RAAN. I have to transfer from a specific point (true anomaly given) of one orbit to a given point of another in 1 month. The period of the ...
Leeloo's user avatar
3votes
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Quantitatively, how deep are the stable equilibrium points in GEO? How much delta-v needed to move from one to the other?

This answer discusses a spacecraft in GEO using a two-impulse (circular → elliptical → circular) raise & lower maneuver to move (phase) itself by 180 degrees in longitude then return to synchrony. ...
uhoh's user avatar
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3votes
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What orbital maneuver(s) did the SOHO have to execute for halo orbit insertion?

I started, but did not complete, Classical Mechanics as an undergraduate, decades ago so I will not understand a highly technical answer. I am writing a novel where an astronaut needs to execute HOI (...
Bob516's user avatar
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Will SpaceX ever be able to launch Starlink Satellites from Boca Chica?

Starlink satellites have orbital inclinations of 43 to 97.6 degrees (but 60% of the satellites orbit at 53*). Launch corridors in the US are over open water to avoid danger to those of us on the ...
Woody's user avatar
2votes
0answers
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Are there any proposals for propulsive debris deorbiting which address basic requirements for efficiency?

This illustration shows many of the challenges using propulsive deorbiting: https://www.smithsonianmag.com/air-space-magazine/34_aug2017-cleaning-up-space-junk-180963932 The trust line of the tug is ...
Woody's user avatar

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