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How much energy would be required to move the earth into a circular orbit with a radius 1.0km larger than its current radius?

Short Answer

Expert verified

Total of1.89×1025Jenergy would be required to move the earth into a circular orbit with a radius1.0km.

Step by step solution

01

Given Information

New radius of the circular orbit is 1.0kmlarger than the current radius.

02

Formula used

Excess energy E=GMm2R-GMm2R+r

Here, gravitational constant G=6.67×10-11N·m2/kg2.

Mass of the sun, localid="1648185717314" M=1.989×1030kg.

Mass of the earth, m=5.97×1024kg.

Initial radius of earth's orbit, localid="1648185813557" R=1.5×1011m.

New radius of earth's orbit,R+r=1.5×1011+103m.

03

:  Calculation

Substitute the values and obtainE.

E=GMm2R-GMm2R+rE=GMm21R-1R+rE=6.67×10-11N·m2/kg2×1.989×1030kg×5.97×1024kg211.5×1011m-11.5×1011m+103mE=39.6×1043×4.78×10-20JE=1.89×1025J
04

Final Answer

Total of1.89×1025Jenergy would be required to move the earth into a circular orbit with a radius1.0km .

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Most popular questions from this chapter

A rocket is launched straight up from the earth’s surface at a speed of 15,000m/s.What is its speed when it is very far away from the earth?

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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.

A moon lander is orbiting the moon at an altitude of 1000 km. By what percentage must it decrease its speed so as to just graze the moon’s surface one-half period later?

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