Questions tagged [reboost]
The reboost tag has no summary.
18 questions
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What are the attitude dynamics of the ISS during a Cygnus reboost?
The International Space Station requires regular reboosting due to its relatively low orbit causing high atmospheric drag. Most of these boosts are performed by the Russian Progress supply vehicle. ...
2
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How to calculate the optimal altitude for an orbital propellant depot
In the current Artemis program, the Starship Human Landing System (HLS) plan calls for the HLS Starship vehicle to be refilled in LEO from an orbiting propellant depot.
If the depot orbits lower, it ...
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How can the ISS be boosted without inducing a spin given its asymmetry? Can the attitude thrusters of a Progress alone counter its main engine? [duplicate]
The ISS has been pushed in the past by Zvezda's two small thrusters (nowadays inactive it seems) and more often by a Progress docked at the back of Zvezda. However the nozzle of the Progress can't ...
4
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What orbit-raising propulsion system will Tiangong use, and how does it differ from that of the ISS in terms of performance and technology?
The new Wall Street Journal video China's Answer to the Aging International Space Station: The Tech Behind Tiangong | WSJ emphasizes after 03:26 that Tiangong's ...
4
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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 ...
4
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2
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Do standard procedures for securing the ISS before an orbital boost burn include making sure that at least large objects are securely "strapped down"?
In discussions on previous posts it was debated whether ISS crew would need to "batten down the hatches" and confirm all objects were "lashed to the deck" before an orbital boost ...
10
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Garbage powered reboosting module for low Earth orbiting space stations
Instead of dumping massive garbage packs once in a while, using a robotic arm, could some sort of garbage canon eject the same mass in small pieces, at higher velocity, so that it contributes to ...
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How hard does atmospheric drag push on the ISS? Is it more than one pound?
A comment under this question has me thinking; with it's huge main structure and giant solar panels the ISS presents a very large cross-section to Earth's rarified atmosphere at 400 km altitude. So ...
3
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Could the Crew Dragon be used to re-boost the ISS?
In an answer to a related question, Jörg W Mittag wrote the following:
But more importantly, handling of the Superdracos is currently rather simple. They are safed after reaching orbit and then never ...
3
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1
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Crew Positioning in ISS during Reboost
Several questions address the reboosting procedure for the ISS. When the shuttle reboosted the station, apparently the entire ISS was modeled on the ground and pre-programmed in, down to the masses ...
11
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How hard was it for the Shuttle to perform attitude control for the entire ISS? Did they have to calibrate?
This answer to the question How was the Space Shuttle Orbiter used for ISS Reboost? describes a procedure I never knew happened. When the shuttle was docked to the ISS it sometimes used its rear ...
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How was the Space Shuttle Orbiter used for ISS Reboost?
According to this answer, for the question How often does ISS require re-boosting to higher orbit?,
During Space Shuttle years, small re-boosts were also performed by the Shuttle Orbiters (...
1
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1
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ISS location identification; estimate size and direction of astronaut acceleration puzzler
note: This question addresses the same video and phenomenon described in this answer (which I found after posting this) but here I'm asking for an analysis of the trajectories of the test masses (the ...
2
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ISS reboost cost
The most updated data available at spaceflight.nasa.gov show that on day 361 there was a reboost:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS)...
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No reboosts for the ISS
The graph shows the ISS semi-major axis.
EDIT: the blue plot represents the ISS mean radius vector minus 6371 km (just to show an approximate altitude), which is equivalent to the sami-major axis (I ...