Motion in 2D astronaut orbiting moon

In summary: In other words, the equation becomes T=2*pi*r*a, where a is the radius of the Earth. So in summary, the satellite is orbiting the Earth at a speed of 7208 m/s, and it will take 92.98 minutes to orbit the Earth once.
  • #1
knightassassin
13
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.
 
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  • #2
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.
 
  • #3
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.
 
  • #4
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.
 
  • #5
what does m stand for?
 
  • #6
generally in physics m stands for mass... and usually when you see 'm' and 'g' together that is a big give away.
 
  • #7
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.
 

FAQ: Motion in 2D astronaut orbiting moon

How does the astronaut maintain a stable orbit around the moon?

The astronaut maintains a stable orbit around the moon by moving at a constant speed and direction, balancing the pull of gravity from the moon and the centrifugal force from the astronaut's motion.

What factors affect the motion of the astronaut in 2D orbit?

The motion of the astronaut in 2D orbit is affected by the mass of the moon, the distance between the moon and the astronaut, and the velocity of the astronaut's orbit.

How does the astronaut change their orbit around the moon?

The astronaut can change their orbit around the moon by adjusting their speed or direction of motion. This can be done by firing thrusters or using gravitational forces from other celestial bodies.

Can the astronaut fall into the moon's gravity well and crash?

Yes, if the astronaut's orbit is not properly maintained or if there are external forces acting on the astronaut, they can fall into the moon's gravity well and crash.

Why does the astronaut appear to be weightless in orbit?

The astronaut appears to be weightless in orbit because they are in a state of free fall, constantly accelerating towards the moon due to the force of gravity. This creates a feeling of weightlessness as there is no contact force pushing back against the astronaut's body.

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