How Long Does a Hohmann Transfer from Earth to Vesta Take?

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In summary, the question asks for the time it would take to travel from Earth to Vesta using a Hohmann transfer orbit during the DAWN mission. The solution involves finding the length of the semimajor axis of the transfer ellipse and using formulas to determine its period.
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yz250fcaptain
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Homework Statement


Hello all in the physics forum!
During the DAWN mission NASA planned to visit Vesta (2.36 AU) and Ceres (2.77AU). Assuming both asteroids are in the eliptic plane, how much time in years would it take by hohmann transfer orbit to travel from Earth to vesta?
I don't expect anyone to solve this but i need some type or direction

Homework Equations



Was giving no further information that what is in the question

The Attempt at a Solution



Dont know where to begin
 
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  • #2
yz250fcaptain said:

Homework Statement


Hello all in the physics forum!
During the DAWN mission NASA planned to visit Vesta (2.36 AU) and Ceres (2.77AU). Assuming both asteroids are in the eliptic plane, how much time in years would it take by hohmann transfer orbit to travel from Earth to vesta?
I don't expect anyone to solve this but i need some type or direction

Homework Equations



Was giving no further information that what is in the question

The Attempt at a Solution



Dont know where to begin

A Hohmann transfer orbit is an ellipse joining two other (usually circular) obits. In this case one orbit is that of the Earth and the other is that of Vesta. The major axis of the ellipse has ends on each orbit, and thus the travel time from one end of the ellipse to the other end is half the period of the whole elliptical orbit with that major axis.

Your job is to determine the length of the semimajor axis of the transfer ellipse, and then using appropriate formulas the period of the ellipse that it describes.
 
Last edited:

What is the Hohmann Transfer Problem?

The Hohmann Transfer Problem is a mathematical problem that involves calculating the most efficient trajectory for a spacecraft to transfer from one circular orbit to another, using the least amount of propellant.

Why is the Hohmann Transfer considered the most efficient transfer method?

The Hohmann Transfer is considered the most efficient transfer method because it requires the least amount of propellant and takes advantage of the natural gravitational forces of the bodies involved.

What are the key assumptions made in the Hohmann Transfer Problem?

The key assumptions made in the Hohmann Transfer Problem are that the orbits of the two bodies are circular and coplanar, and that the spacecraft is small compared to the bodies involved.

How do you calculate the timing of a Hohmann Transfer?

To calculate the timing of a Hohmann Transfer, you need to know the orbital periods of the two bodies and the ratio of their radii. The transfer will occur when the spacecraft is at the point where its orbit intersects the target orbit.

What are some real-world applications of the Hohmann Transfer?

The Hohmann Transfer is commonly used in space missions, such as satellite launches and interplanetary missions. It is also used for orbital maneuvers and rendezvous between spacecrafts.

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