Space station artificial gravity - how to spin up to speed?

Click For Summary

Discussion Overview

The discussion revolves around methods for spinning up a space station to create artificial gravity, focusing on the feasibility and implications of using reaction wheels, counter-rotating systems, and traditional thrusters. Participants explore various mechanical configurations and their effects on station orientation and operational flexibility.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested
  • Mathematical reasoning

Main Points Raised

  • Some participants suggest using attitude rockets for spinning the station, though they express concerns about fuel consumption and future maneuverability.
  • Others propose using a reaction wheel, either mounted inside or outside the station, to counteract gyroscopic effects and facilitate orientation.
  • There are considerations about the mass and size of the reaction wheel, with some arguing that a larger wheel could reduce the effective mass but might complicate spacecraft docking.
  • Participants discuss the potential for spinning different parts of the station in opposite directions as an alternative, noting the lack of additional mass for a wheel but raising safety concerns for crew movement between sections.
  • Some contributions highlight the energy requirements for various methods, comparing the efficiency of chemical rockets versus ion thrusters for achieving the necessary spin rates.
  • There are questions about the practicality of connecting systems across rotating sections and the implications for crew safety and operational logistics.

Areas of Agreement / Disagreement

Participants express a range of views on the best method for achieving artificial gravity, with no consensus reached. While some favor traditional thrusters, others advocate for reaction wheels or counter-rotating systems, highlighting the complexity and trade-offs involved in each approach.

Contextual Notes

Participants note various assumptions regarding mass, energy efficiency, and operational flexibility, but these remain unresolved. The discussion includes considerations of angular momentum conservation and the implications of different configurations on station stability and safety.

Who May Find This Useful

This discussion may be of interest to those exploring engineering solutions for space habitats, particularly in the context of artificial gravity and spacecraft design challenges.

  • #151
sophiecentaur said:
The illusion of gravity is limited. If you release an object from the periphery it will not follow a path that appears to be vertically 'downwards'
On the contrary. It will follow a path that appears to be vertically downwards -- at least until it attains a velocity significant enough for Coriolis to rear its head.

If you are standing in front of the counter on a space station trying to make an omelette and you drop an egg, it will land on the floor at your feet -- to a first approximation.
 
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  • #152
A.T. said:
Show your work.

I can't draw diagrams on my iPhone, I'm afraid but my description of the diagram is reasonably accurate.
Must reconsider, I think.
 
  • #153
sophiecentaur said:
I can't draw diagrams on my iPhone
What radius and tangential velocity did you assume to get that 1m separation after 1s?
 
  • #154
30 meters/sec on a 100 meter radius is 0.3 radians after 1 second. Cos of 0.3 radians is 0.955. That's 4.5 meters separation. As expected for 0.9 gee by SUVAT.

Edit: ##\frac{v^2}{r}## is 9.0 meters/s2 for that setup.
 
  • #155
That figure I came up with was clearly rubbish (back of envelope let me down - sorry chaps) and the distance would be something like 4.5m. But that approach was totally unsuitable. What needs to be considered is how to deal with the effect of a step function of 0 to 1 g. This is the equivalent of what the suspension has to deal with if you suspend a car with its wheels not quite touching the ground and then let go. That is a trivial requirement and all cars will cope easily with that. It's essential for protecting the road surface as much as anything. The advantage for the docking mechanism is that it can afford to move much more than a car suspension. It can be a lot softer and would involve a much lighter weight mechanism. And, of course, from what's been written here, we are talking in terms of g/5, rather than g.
 
  • #156
Al_ said:
If a space station has artificial gravity created by spinning, how can it best be spun up to speed? Little attitude rockets could do it, but they would use up fuel, and limit your ability to change the spin rate in future. What if you had an external wheel that you spin up very fast in the opposite direction? If you did this, would it cancel out the gyroscope effect because the total angular momentum of the whole would be zero, and make it easier to orient the station with respect to the Sun, spacecraft , etc.?

Could Feraday's Law of Induction be employed to generate sufficient energy to sustain gyroscopic motion? Would this effectively produce a perpetual motion device? I picture a system of tubes within the structure of the gyroscope. I'm thinking, though, that the structure would be to large to be practical.
 
  • #157
David Pass said:
Could Feraday's Law of Induction be employed to generate sufficient energy to sustain gyroscopic motion?
Using induced voltages would slow the rotation. That is the opposite of what we want.

You could use electric power (from solar cells) to induce a current in a tether, and use that to generate torque. JAXA tried that recently, although not for rotation.
David Pass said:
Would this effectively produce a perpetual motion device?
There is no such thing.
 
  • #158
Has anyone considered doing penetrating ground radar? Is it possible the moon or Mars has fossil fuel like we do? If so couldn't that be used to run the artificial gravity mechanism?
 
  • #159
Fossil fuels come from long dead life forms. There is no evidence (or reason to believe) that the Moon had life at any time.
 
  • #160
And even if there would be hydrocarbons, there is no free oxygen to burn it.

Artificial gravity is interesting in space, but not so much on Moon/Mars.
 
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