Hohmann transfer orbit
A Hohmann Transfer Orbit is an efficient way to move a spacecraft between two circular orbits around a planet or the Sun. It involves two engine burns: the first to increase the spacecraft's speed, allowing it to enter an elliptical orbit that reaches the higher orbit, and the second burn at the highest point to circularize the orbit. This method minimizes fuel usage and is commonly used for missions between planets, making it an essential concept in space travel and orbital mechanics. It takes advantage of the gravitational mechanics to optimize travel time and energy.
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A Hohmann transfer orbit is a fuel-efficient way to move a spacecraft between two different orbits around a planet or between planets. It involves two engine burns: the first to leave the starting orbit and enter an elliptical path that touches the target orbit, and the second to circularize the orbit at the destination. This method minimizes the energy required for the transfer, making it an economical choice for space missions. It's commonly used for missions to Mars, satellites, and other celestial bodies.