G-Force Measurement: Formulas for Launching into Orbit

AI Thread Summary
The discussion centers on g-force measurement during satellite launches, highlighting that 1 G is experienced at ground level, with 3-5 G during launch, and 0 G in orbit. Participants clarify that g-force is influenced by the acceleration applied, which must exceed 9.8 m/s² to achieve lift-off. There is debate over the exact g-force experienced during launch, with estimates varying between 2 G and 3 G based on different acceleration values. A participant suggests consulting Wikipedia for formulas related to g-force calculations. Overall, understanding the relationship between acceleration and g-force is crucial for analyzing launch dynamics.
Sword7
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Hello folks,

Does anyone know any formula about g-force measurement when launching into orbit? For example, 1 G at ground, 3-5 G during launching, 0 G at orbit.

Thanks,
Tim
 
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Hi,
I don't think there's a general formula. For example it could be say "500 G" for a little time (launching time) and then you could put the satellite into orbit.
It could also be accelerated very slowly, so G wouldn't get higher than "2 G" during its trip from Earth's ground to Earth's orbit.
But in any case you need to accelerate the satellite more than g (that is, around 9.8m/s^2).
 
Sword7 said:
Hello folks,

Does anyone know any formula about g-force measurement when launching into orbit? For example, 1 G at ground, 3-5 G during launching, 0 G at orbit.

Thanks,
Tim

One G equals to 9.8m/s2. You have 1 G at the surface of the Earth as well. So before launching, the g-force is 1 G (just like you and me have). At the launch, if the acceleration is ~20m/s2 so the astronauts bear about 3 G , and so on. In orbit, the g-force is almost zero and you have O G.
 
pixel01 said:
One G equals to 9.8m/s2. You have 1 G at the surface of the Earth as well. So before launching, the g-force is 1 G (just like you and me have). At the launch, if the acceleration is ~20m/s2 so the astronauts bear about 3 G , and so on. In orbit, the g-force is almost zero and you have O G.

Are you sure pixel, that if the acceleration is about 20m/s^2 then the astronauts bears 3 G?
I wouldn't say so. For me it's about 2 G. Even if the force required to do so has to "cancel out" the "1 G" acceleration we feel on Earth's ground and then has to propulse the astronauts to an acceleration of 20 m/s^2.
 
Pixel is correct. Relative to a free-falling reference frame, that rocket is accelerating upward at about 30 m/s^2, not 20.
 
D H said:
Pixel is correct. Relative to a free-falling reference frame, that rocket is accelerating upward at about 30 m/s^2, not 20.

Ok then I'm wrong.
I get it now!
 
Hello folks,

I found equation for g-force when I searched through google. Look at http://en.wikipedia.org/wiki/G-force" about equation of g-force for calculation.

Tim
 
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