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Pluto moves in a fairly elliptical orbit around the sun. Pluto’s speed at its closest approach of 4.43×109km is 6.12 km/s. What is Pluto’s speed at the most distant point in its orbit, where it is7.30×109km from the sun?

Short Answer

Expert verified

The Pluto's speed at the most distant point in its orbit is3.71km/s.

Step by step solution

01

Step 1. Given information

Here,

r1=³¦±ô´Ç²õ±ð²õ³Ù»å¾±²õ³Ù²¹²Ô³¦±ð=4.43×109kmv1=speedatclosestdistance=6.12km/sr2=´Ú²¹°ù³Ù³ó±ð²õ³Ù»å¾±²õ³Ù²¹²Ô³¦±ð=7.30×109kmv2=?
02

Step 2. Formula used

Angular momentum, L=mvr

where,

m=mass of planet

r=distance from sun

v=speed of planet

03

Step 3. Calculation

As angular momentum should remain constant.

mv1r1=mv2r2⇒v2=v1r1/r2⇒v2=4.43×109×6.127.30×109km/s⇒v2=3.71km/s

04

Step 4. Conclusion

The speed of pluto at most distant point is 3.71km/s.

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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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