Two 65kgastronauts leave earth in a spacecraft, sitting 1.0mapart. How far are they from the center of the earth when the gravitational force between them is as strong as the gravitational force of the earth on one of the astronauts?

Short Answer

Expert verified

The astronauts are 3.03×1011maway from the center of the earth when the gravitational force between them is as strong as the gravitational force of the earth on one of the astronauts.

Step by step solution

01

Given information.

Mass of the astronauts = 65kg, distance between them = 1m.

02

Calculation.

Here,

Mass of the astronauts m1=m2=65kg.

Separation between astronauts r12=1.0m.

Mass of earth localid="1648480144458" Me=5.97×1024kg.

Therefore, the force between the astronauts :F1=G×m1×m2×r12×2.

03

Continuation of calculation.

Consider the distance of the astronauts from the centre of earth is r.

So, the gravitational force between earth and astronaut is :

F2=GM2m1r2.

Now equate the above two equations and solve for r.

Gm1m2r122=GMem1r2m2r122=Mer2r2=Mem2r122r=Mem2r12.

Now substitute the values of Me,m2and r12to calculater:

localid="1648480176345" r=(5.97×1024kg)(65kg)(1.0m)=3.03×1011m.

04

Final answer.

The astronauts are 3.03×1011maway from the center of the earth when the gravitational force between them is as strong as the gravitational force of the earth on one of the astronauts.

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Planet Z is 10,000kmin diameter. The free-fall acceleration on Planet Z is role="math" localid="1648089747827" 8.0m/s2.

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Let’s look in more detail at how a satellite is moved from one circular orbit to another. FIGURE CP13.71shows two circular orbits, of radii localid="1651418485730" r1and localid="1651418489556" r2, and an elliptical orbit that connects them. Points 1and 2are at the ends of the semimajor axis of the ellipse.

a. A satellite moving along the elliptical orbit has to satisfy two conservation laws. Use these two laws to prove that the velocities at points localid="1651418503699" 1and localid="1651418499267" 2are localid="1651418492993" v1=2GMr2/r1r1+r2and localid="1651418509687" v2=2GMr1/r2r1+r2The prime indicates that these are the velocities on the elliptical orbit. Both reduce to Equation 13.22if localid="1651418513535" r1=r2=r.

b. Consider a localid="1651418519576" 1000kgcommunications satellite that needs to be boosted from an orbit localid="1651418573632" 300kmabove the earth to a geosynchronous orbit localid="1651418578672" 35,900kmabove the earth. Find the velocity localid="1651418584351" v1on the inner circular orbit and the velocity localid="1651418590277" v=1at the low point on the elliptical orbit that spans the two circular orbits.

c. How much work must the rocket motor do to transfer the satellite from the circular orbit to the elliptical orbit?

d. Now find the velocity localid="1651418596735" v=2at the high point of the elliptical orbit and the velocity v2 of the outer circular orbit.

e. How much work must the rocket motor do to transfer the satellite from the elliptical orbit to the outer circular orbit?

f. Compute the total work done and compare your answer to the result of Example localid="1651418602767" 13.6.

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