EBK LOOSE-LEAF VERSION OF UNIVERSE
EBK LOOSE-LEAF VERSION OF UNIVERSE
11th Edition
ISBN: 9781319227975
Author: KAUFMANN
Publisher: VST
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Chapter 7, Problem 13Q

(a)

To determine

The escape speed of a spacecraft from Europa (Jupiter’s moon), which revolves around an orbit of radius 670900 km. Given that the spacecraft, after collecting the sample from the satellite’s surface, is returning to Earth.

(a)

Expert Solution
Check Mark

Answer to Problem 13Q

Solution:

2.02 km/s

Explanation of Solution

Given data:

A spacecraft landed on Jupiter’s moon, which revolves around Jupiter in an orbit of radius 670900 km.

Formula used:

The relation for the escape velocity is as:

vescape=(2GMR)12

Here, vescape is the escape velocity for Europa, G is the universal gravitational constant having value 6.67×1011 Nm2/kg2, M is the mass of Europa and R is the radius of Europa.

Explanation:

Mass of Europa is 4.80×1022 kg and its radius is 1.57×106 m .

Recall the above formula.

vescape=(2GMR)12

Substitute 4.80×1022 kg for M, 1.57×106 m for R and 6.67×1011 Nm2/kg2 for G

vescape=(2(6.67×1011 Nm2/kg2)(4.8×1022 kg)1.57×106 m)12=(6.4032×10121.57×106 m)12=(4.07×106)12=2.02×103 m/s

vescape=2.02×103 m/s(km1000 m)=2.02 km/s

Conclusion:

Therefore, the escape velocity to leave Europa is 2.02 km/s.

(b)

To determine

The escape speed from Jupiter at the distance of Europa’s orbit, if a spacecraft landed on Jupiter. Given that the orbit of Europa has a radius of 670900 km.

(b)

Expert Solution
Check Mark

Answer to Problem 13Q

Solution:

19.28 km/s

Explanation of Solution

Given data:

A spacecraft landed on Jupiter’s moon, which moves around Jupiter in an orbit of radius 670900 km.

Formula used:

The relation for the escape velocity is as:

(vescape)jupiter=(2Gmr)12

Here, (vescape)jupiter is the escape velocity for Jupiter, G is the universal gravitational constant having value 6.67×1011 Nm2/kg2, m is the mass of Jupiter and r is the radius of Jupiter.

Explanation:

The mass of Jupiter is 1.89×1027 kg and the radius of Jupiter is 6.78×108 m .

Recall the above formula.

(vescape)jupiter=(2Gmr)12

Substitute 1.89×1027 kg for m, 6.78×108 m  for r and 6.67×1011 Nm2/kg2 for G

(vescape)jupiter=(2(6.67×1011 Nm2/kg2)(1.89×1027 kg)6.78×108 m)12=(2.52×10176.78×108 m)12=(371.86×106)12=19.28×103 m/s

(vescape)jupiter=19.28×103 m/s(km1000 m)=19.28 km/s

Conclusion:

Therefore, the escape speed from Jupiter at the distance of Europa’s orbit is 19.28 km/s.

(c)

To determine

The explanation that the space craft must leave Europa with a speed greater than the speed, which is calculated in part (a) or part (b), in order to begin its homeward journey if the spacecraft landed on Jupiter’s moon, which revolves around Jupiter in an orbit of radius 670900 km. After collecting the sample from the satellite’s surface, the spacecraft prepares its return to Earth.

(c)

Expert Solution
Check Mark

Answer to Problem 13Q

Solution:

The large escape velocity is required, to cross Jupiter, as compared to Europa’s escape velocity.

Explanation of Solution

Introduction:

Escape velocity: The lowest velocity which is required by the body to escape the gravitational attraction of a particular planet is known as its escape velocity.

Explanation:

The escape velocity for Europa is 2.02 km/s, which is calculated in the part (a) and the escape velocity for Jupiter is 19.28 km/s, which is calculated in part (b).

From the above calculations, it can be observed that the escape velocity for Europa is less than the escape velocity for Jupiter. If a spacecraft achieves a velocity which is equal to the escape velocity of Europa, then the spacecraft cannot cross the Jovian system. There is requirement of larger velocity than the escape velocity of Europa, to escape the Jovian system for the spacecraft.

Conclusion:

Therefore, for the spacecraft to escape from the Jovian system, an escape velocity larger than that of Europa is required.

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