Motion in 2D astronaut orbiting moon

Click For Summary

Homework Help Overview

The discussion revolves around an astronaut preparing to dock with a satellite in orbit around the Earth. The problem involves calculating the speed of the satellite and the time required for one complete orbit, given specific parameters such as the altitude of the satellite and the acceleration due to gravity at that altitude.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • Participants explore the relationship between radial acceleration and velocity, questioning the relevance of certain calculations. There is an attempt to clarify the objective of the problem and the correct radius to use for calculations. Some participants discuss the implications of mass in the equations presented.

Discussion Status

The discussion is ongoing, with participants providing clarifications and questioning assumptions. Some guidance has been offered regarding the use of gravitational acceleration and the radius for calculations, but no consensus has been reached on the correct approach to the problem.

Contextual Notes

Participants note the importance of using the correct radius for calculations and the implications of gravitational acceleration at the satellite's altitude. There is also a mention of unit consistency as a potential concern.

knightassassin
Messages
13
Reaction score
0

Homework Statement


The astronaut orbiting the Earth in Figure P4.32 is preparing to dock with a Westar VI satellite. The satellite is in a circular orbit 700 km above the Earth's surface, where the free-fall acceleration is 8.12 m/s2. Take the radius of the Earth as 6400 km. 2. Relevant equations
T=2(pi)radius/velocity
radial acceleration=V^2/radiusI am not sure if this is relevant, but the distance from the the satellite to the center of the Earth is 6400km+700km=7100km.
Next I try to find the time it takes the satellite to reach the center:
First I find velocity from the radial acceleration equation. I set a=8.12m/s^2 (not sure if this is right)
Next I solve for velocity=sqrt(a*r) where r=6400
v=7208m/s
Next I use the velocity to calculate the time it takes for the object to reach the center using the equation T=2(pi)radius/velocity
=2pi*6400000/7208
=92.98 min (I already converted it back to minutes from seconds)

I am not sure what I am doing wrong.
 
Physics news on Phys.org
Err, what is the objective of all of this? To find the time it takes for the object to reach the center? The center of what?

What does the question ask you to solve?

And just from looking at your r, you seem to be using the r that is at Earth's surface, not the actual one you calculated above.
 
whoops, sorry I forgot that part

a) Determine the speed of the satellite.
b)Determine the time interval required to complete one orbit around the Earth.
 
knightassassin said:
whoops, sorry I forgot that part

a) Determine the speed of the satellite.
b)Determine the time interval required to complete one orbit around the Earth.

They give you gravity at that altitude, so that makes it simpler.

m*g' = m*v2/ r

Where r = 6400 + 700 = 7100 km

Careful of units.
 
what does m stand for?
 
generally in physics m stands for mass... and usually when you see 'm' and 'g' together that is a big give away.
 
knightassassin said:
what does m stand for?

As djeitnstine has pointed out, it is mass.

Before you ask what it is for the satellite, notice that whatever it is cancels out.
 

Similar threads

  • · Replies 5 ·
Replies
5
Views
2K
  • · Replies 3 ·
Replies
3
Views
2K
Replies
5
Views
3K
Replies
6
Views
3K
  • · Replies 1 ·
Replies
1
Views
3K
Replies
37
Views
4K
  • · Replies 10 ·
Replies
10
Views
4K
  • · Replies 5 ·
Replies
5
Views
2K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 1 ·
Replies
1
Views
2K