Insufficient Data: Calculating Orbital Energy Gain

In summary, a student came across a question during their exam review about the energy added to the orbit of the International Space Station by the space shuttle. They were unsure of how to solve it without knowing the mass of the satellite, and sought guidance from a classmate. Through a series of equations and calculations, it was determined that the mass of the ISS is necessary to accurately solve the question, but it is not a requirement for an exam question. The current mass of the ISS is 187,000 kg, but it will continue to increase as more components are added.
  • #1
Parth Dave
299
0
Came across another question during my exam review. Seems to me like there is insufficient data again.

When the space shuttle delivers a crew to the international space station, it usually boosts the orbit of the station from about 320 km to 350 km. How much energy does the shuttle add to the stations orbit?

Orbital energy is given as:
E = -GMm/(2r)

The energy gain would be the difference from the initial energy and final energy. But how can you solve it without being given the mass (ans is 1.48E10 J)?
 
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  • #2
yes, you can't solve this without the mass... try google it...see if you have luck...
 
  • #3
Whose mass??The satellite's??Or the Earth's?

Daniel.

P.S.Set the equations properly and see what data is missing.
 
  • #4
Energy the shuttle added = change in potential energy
Therefore,

E = -GMm/2(rf) - -GMm/2(ri)
= GMm/2 * (1/(ri) - 1(rf))

Where m = mass of the space station, M = mass of earth

Everything is given except m.
 
  • #5
The current mass of the ISS is 187,000 kg. Don't count on that giving you the right answer. The question will only work out if you know what the mass of the ISS was on the date the question was written. That's going to take quite a bit of googling. Granted, with the halt in shuttle flights, the mass has stayed reasonably constant for awhile, now, but the mass will start increasing again as soon as they start taking more major components up to it.

When all the segments have been completed, launched, and assembled, it will have a mass of 417,000 kg (down from about 470,000 kg thanks to a few canceled projects).

Of course, no matter how many segments are added, the specific energy per unit of mass will stay the same. If you want to analyze the motion of the ISS, the specific energy will do since the acceleration due to gravity is the same regardless of the mass (but the specific energy won't match your answer, either).

(This question is almost as challenging as determing the amount of potential energy gained by taking Oprah up Mt Everest, isn't it?)
 
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  • #6
Thx alot! Although I'm not concerned about the question. I just wanted to make sure I was correct in assuming the mass was necessary. No exam question will ever require you to know the mass of the ISS. Btw, the 187,000 kg gives an answer pretty close to what they wanted.
 
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Related to Insufficient Data: Calculating Orbital Energy Gain

1. What is "Insufficient Data: Calculating Orbital Energy Gain"?

"Insufficient Data: Calculating Orbital Energy Gain" is a scientific concept that refers to the process of determining the amount of energy gained by an object as it moves in an orbital path around another object, such as a planet or star.

2. How is orbital energy gain calculated?

Orbital energy gain is calculated using the formula E = -GMm/2r, where E is the energy gained, G is the gravitational constant, M is the mass of the larger object, m is the mass of the smaller object, and r is the distance between the two objects.

3. Why is there sometimes insufficient data for calculating orbital energy gain?

Insufficient data can occur for a variety of reasons, including limited observational data, incomplete knowledge of the masses or distances of the objects, or the presence of other unknown variables that may affect the calculations.

4. How can scientists overcome insufficient data when calculating orbital energy gain?

Scientists can use various methods to overcome insufficient data, such as collecting more accurate measurements, using advanced mathematical models, or incorporating data from other sources or related studies.

5. What are some real-world applications of calculating orbital energy gain?

Calculating orbital energy gain has many practical applications, including predicting the trajectories of space objects such as satellites, spacecraft, and planets, as well as understanding the stability of binary star systems and other celestial bodies.

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