Satellite - resistance (retarding force)

AI Thread Summary
The discussion centers on calculating the average resistance force acting on a satellite with a mass of 3000 kg at an altitude of 300 km. Participants note that at this height, atmospheric resistance is negligible due to the lack of air. The conversation highlights the importance of the full problem statement, as the context of the satellite's flight—whether in low orbit or during launch—affects the relevance of resistance calculations. It is concluded that for a satellite in stable orbit, the resistive force can be considered zero, while launch scenarios may require further analysis. Clarification from the teacher is suggested for a complete understanding of the problem.
charlie05
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Homework Statement


What is the average resistance force F acting on the satellite during its flight, m = 3000kg, h=300km.

Homework Equations

The Attempt at a Solution


If it is llow orbit, so it inhibits the resistance of the atmosphere. In 300 km is no air, so no resistance ...?
 
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What equation are you using to calculate air pressure at 300 km ?
 
upload_2017-3-20_13-0-21.png
?
 
p0 = 101 325 Pa
h= 300 000m
g=9,81 m/s2
ρ 0 = 1,225 kg/m3
 
p 300 000 = 101 325*e-35,58 Pa
 
https://www.avs.org/AVS/files/c7/c7edaedb-95b2-438f-adfb-36de54f87b9e.pdf
 
Agree it isn't much. What is the question (the full problem statement) ?
 
Yes I agree. Therefore, I think that is a resistive force is zero.
 
BvU said:
What is the question (the full problem statement) ?
According to your terse problem statement they ask for the average reisistance during its flight.
If its flight is circling the Earth for 30 years it might be relevant to come up with a non-zero number.
But if its flight is a launch from sea level all the way up to 300 km I suppose you can ignore the pressure up there.

That's why I asked for the full problem statement
 
  • #10
I understand. I have to ask my teacher. Yet I thank you for the effort and help.
 
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