Help with Problems: Solve & Estimate Time Needed

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Homework Help Overview

The discussion revolves around a problem involving a satellite orbiting Mars and its energy requirements to escape the planet's gravitational field. The context includes calculations related to gravitational potential energy, solar energy collection, and orbital mechanics.

Discussion Character

  • Exploratory, Assumption checking, Problem interpretation

Approaches and Questions Raised

  • Participants are examining the relationship between the energy collected by the satellite and the gravitational potential energy needed to escape Mars. Questions arise about the definition of "enough energy" and how solar radiation contributes to this energy requirement. There is also a focus on the implications of the satellite being in Mars' shadow.

Discussion Status

The discussion is ongoing, with participants seeking clarification on the energy calculations and the impact of the satellite's position relative to the Sun. Some guidance has been offered regarding the energy equations, but no consensus has been reached on the specific calculations or assumptions involved.

Contextual Notes

There are constraints regarding the clarity of the problem statement, particularly concerning what constitutes "enough energy" and the effects of the satellite's orbital position. Participants are encouraged to provide their previous work to facilitate more targeted assistance.

Mateja
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Can you help me with solving this few problems>

1. Satellite is orbiting above the Mars at 6 600 km above the surface. On the satellite are solar discs who are gathering energy from Sun. If the surface of all discs is 50 m^2, estiamte how much time is enough to satellite gath enough energy to live gravitational field of Mars. How much time (n) satellit orbits the planet for this time? Part of energy that accumulate is 80% of energy of Sun radiation that falles on the discs. Level of orbite, and solar discs of satellite are always normal on direction Mars-Sun. Mmars = 0,64 x 10^24 kg, Rmars = 3 395 km, Msatellite = 3 000 kg, G = 6,67 x 10^-11 Nm^2\kg^2

the rest problems I will post later...
 
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This looks like homework so I am moving it. Also, Mateja, you must post what you have done on this so we will know what kind of help you need.
 
If the surface of all discs is 50 m^2, estiamte how much time is enough to satellite gath enough energy to live gravitational field of Mars.

Enough energy for what? I don't see what the gravitational field has to do with "enough energy" for anything.
 
Energy that satellit accumulate must be bigger or equal with gravitational potential energy of Mars, so satellit can leave gravitational field of Mars.

Satellit on circuling around the Mars have energy -G*M*m/(2*a) where a is the semimajor axis of orbit = Rmars + h. Than i don't know hot to get energu from sun radiation, but then i probably must multiplie that energy with 0,8 (80%) and equal it with energy -G*M*m/(2*a). From T=2*pi*a/v, v=sqrt G*M/a and n=t/T i get n. i have two problems

1. how to get energy of sun radiation
2. wath will hapen when satellite is in Mars shadow
 

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