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tandoorichicken
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How do you calculate the period of orbit for an elliptical orbit, ie, a Hohmann transfer?
A Hohmann transfer orbit is an elliptical orbit used by spacecraft to transfer between two circular orbits of different altitudes. It is the most fuel-efficient way to transfer between two orbits.
A Hohmann transfer orbit works by using the gravitational pull of a planet or other celestial body to change the spacecraft's velocity and transfer it from one circular orbit to another. This is achieved by firing a thruster at precise points along the orbit.
The duration of a Hohmann transfer orbit is affected by the distance between the two orbits, the mass of the spacecraft, and the thrust of the spacecraft's engines. The closer the two orbits are, the shorter the transfer time will be.
The main advantage of using a Hohmann transfer orbit is that it requires the least amount of fuel compared to other transfer methods. It also allows for a precise and predictable transfer between orbits.
One limitation of a Hohmann transfer orbit is that it is only applicable for transferring between circular orbits. Additionally, it may not be the most efficient method for transferring between orbits with a large difference in inclination or when time is a critical factor.