New orbit of satellite deflected by Jupiter

In summary, the new aphelion is 13.1km/s from Jupiter, the perihelion is 5.7km from Jupiter, and the orbital period is 9.5 hours.
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Dazed&Confused
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Homework Statement


This question involves parts of other questions, so I will state the relevant parts and essentially what the question is asking. It is from Kibble Classical Mechanics, Chapter 4, Question 22. If more information is needed I will provide.

We have a satellite that orbits the sun initially. It's orbit extends from Earth's to Jupiter's and it just touches both. Thus the speed of the satellite when near Jupiter is 7.4km/s while that of Jupiter is 13.1km/s. The satellite is deflected by Jupiter by 90 degrees in Jupiter's frame of reference so that in this frame the satellite ends up traveling away from the Sun. Thus in the frame of reference of the Sun the satellite is now traveling at 13.1km/s tangentially and 5.7km/s radially. The question asks you to find the new aphelion, perihelion, and orbital period.

Homework Equations


[tex] \tfrac12 m \dot{r}^2 + \frac{J^2}{2mr^2} + V(r) = E[/tex]

The Attempt at a Solution


To me it appears that the energy of the satellite is now positive: the energy of Jupiter was zero (assuming a circular orbit) and now the satellite has the same tangential speed, same potential, but also extra radial speed. Thus the new orbit should be a hyperbola.
 
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  • #2
Dazed&Confused said:
To me it appears that the energy of the satellite is now positive: the energy of Jupiter was zero (assuming a circular orbit) and now the satellite has the same tangential speed, same potential, but also extra radial speed. Thus the new orbit should be a hyperbola.

Perhaps you were thinking of the eccentricity being zero for a circular orbit? Bound orbits (such as those for planets) have negative mechanical energy. Jupiter's specific mechanical energy is:
$$\xi = \frac{v^2}{2} - \frac{\mu}{r}$$
$$ ~~~= \frac{(13.1~km/s)^2}{2} - \frac{(1.327 \times 10^{20}~m^3s^{-2})}{778.3 \times 10^6~km} = -8.47 \times 10^7~J/kg$$

The borderline case of a parabolic orbit has zero mechanical energy.

[edit: fixed math error. Sorry about that!]
 
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  • #3
I feel a bit silly about that. Thanks.
 

1. How does Jupiter's gravity affect the orbit of a satellite?

Jupiter's massive size and strong gravitational pull can significantly affect the orbit of a satellite passing near it. The satellite may experience changes in speed, direction, and position due to the gravitational pull of Jupiter.

2. Can the deflection of a satellite's orbit by Jupiter be predicted?

Yes, the deflection of a satellite's orbit by Jupiter can be predicted using mathematical equations and advanced computer simulations. However, the exact amount of deflection may vary depending on several factors such as the speed, mass, and distance of the satellite from Jupiter.

3. How does the deflection of a satellite's orbit by Jupiter impact its mission?

The deflection of a satellite's orbit by Jupiter can have both positive and negative impacts on its mission. On one hand, it can provide valuable data and insights about Jupiter's gravitational field. On the other hand, it may require adjustments in the satellite's trajectory to ensure it stays on track to complete its mission objectives.

4. Are there any potential risks associated with a satellite's orbit being deflected by Jupiter?

Yes, there are potential risks associated with a satellite's orbit being deflected by Jupiter. If the deflection is too significant, it could potentially cause the satellite to collide with Jupiter or other nearby objects. Furthermore, the deflection may also disrupt communication and data transmission between the satellite and its control center on Earth.

5. How do scientists monitor and track the deflection of a satellite's orbit by Jupiter?

Scientists use a combination of ground-based telescopes and space-based instruments to monitor and track the deflection of a satellite's orbit by Jupiter. By analyzing the satellite's position and trajectory data, they can determine the amount and direction of the deflection and make necessary adjustments to ensure the success of the mission.

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