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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.

2votes
1answer
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Lambert's problem without collisions

Given two fixed positions in space, a source of gravity and a time of flight to travel, the theory about Lambert's problem provides a way to calculate corresponding Keplerian orbital transfers. But, ...
darksun's user avatar
3votes
1answer
116views

Is it possible to use a solar sail in low Earth orbit, thanks to a good orientation of the sail?

I was reading this question: What is the closest to Earth you can expect lift from a solar sail? PearsonArtPhoto’s answer states that below 900 km, a solar sail cannot work because the drag on the ...
AoooR's user avatar
2votes
1answer
184views

How is the Soyuz's movement along the axes ensured using maneuvering engines?

The maneuvering engines are located outside the ship's center of mass and when turned on, they should create rotation, not movement.
user64954's user avatar
13votes
5answers
3kviews

What are the use cases and challenges for a cubesat that would take pictures of other satellites?

I am currently working with a university team in designing a cubesat. I would like to propose to the team that we design a satellite that is able to take pictures of other satellites orbiting nearby. ...
Brandon Sharp's user avatar
2votes
0answers
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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
5votes
1answer
881views

New Glenn and Starship testing approach differences

SpaceX has been doing suborbital flights with Starship for a while now, and intends to conduct a second in-orbit engine re-light to demonstrate de-orbit capability. Blue Origin's New Glenn has flown ...
Ahmed Tawfik's user avatar
3votes
0answers
76views

Calculation of a rendezvous from an elliptical orbit to another [duplicate]

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
12votes
2answers
4kviews

Am I actually escaping Earth?

I am writing a hard-SF story where a spacecraft gets into an highly elliptical earth orbit, having its perigee at 400km but its apogee at 32 000 km (to get close to the asteroid Apophis when it ...
TheYoloToto's user avatar
9votes
1answer
3kviews

Why is China's Tiangong space station inaccessible from Russia's launch sites?

I was reading Ars Technica's 9/21/2024 "NASA has a fine plan for deorbiting the ISS—unless Russia gets in the way". The article states: Russian and Chinese leaders have fostered closer ties ...
Rodo's user avatar
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7votes
2answers
2kviews

What do these expressions mean in NASA's Steve Stitch's brief Starliner undocking statement?

After about 00:30 in The BBC's September 7, 2024 Boeing Starliner returns to earth without astronauts | BBC News, there's a clip of Steve Stitch, Manager, NASA Commercial Crew Program reading a brief ...
uhoh's user avatar
  • 153k
4votes
1answer
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GMAT Lambert problem

I would like to plan a mission in GMAT to a certain asteroid, whose orbit and SPK file I have added in GMAT. However, I don't know how to solve the Lambert problem in it to first find the intersection ...
Arkadiusz Hess's user avatar
1vote
0answers
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Interpreting phasing maneuver results using electric propulsion in GMAT

I'm trying to simulate an anomaly phasing maneuver in three different scenarios using electric propulsion in GMAT. The idea is to use the altitude difference (of ~7-8km) between two spacecrafts to ...
Shawn Lim's user avatar
0votes
0answers
275views

Is it possible to have a closed(-ish) natural motion circumnavigation around an eccentric target? If so, what parameters define the NMC orbit?

Natural motion circumnavigation (NMC) is when a chaser spacecraft is set in an orbit similar to a target spacecraft's such that the chaser naturally circumnavigates the target spacecraft as a result ...
NeutronStar's user avatar
6votes
1answer
117views

E/I separation for GEO statellites

Two GEO satellites are being colocated using the E/I separation method. Typically, the eccentricity vector would trace a circular motion with the circle positioned in the first quadrant of the Ex-Ey ...
Hoang Viet's user avatar
3votes
0answers
94views

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

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