Difference between revisions of "Orbit"
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==LEO== | ==LEO== | ||
| − | Low Earth Orbit is the minimum height (160 km) and velocity (8 km/s) that an object needs to stay in orbit round [[Earth]]. This orbit is the easiest to reach with currently available [[rocketry]]. It might be used to assemble a large spaceship from smaller parts that are lifted separately from Earth. | + | Low Earth Orbit is the minimum height (160 km) and velocity (8 km/s) that an object needs to stay in orbit round [[Earth]]. This orbit is the easiest to reach with currently available [[rocketry]]. It might be used to assemble a large spaceship from smaller parts that are lifted separately from Earth. LEO is subject to drag from the Earth's atmosphere and vehicles in LEO need to be booster periodically to avoid orbital decay and re-entry. |
| − | == LMO == | + | ==LMO== |
Low Mars orbit. Effect of Mars shape. Effect of Mars atmosphere. | Low Mars orbit. Effect of Mars shape. Effect of Mars atmosphere. | ||
| − | == | + | ==Hohmann transfer orbit== |
| + | In orbital mechanics, the '''Hohmann transfer orbit'''<ref>https://en.wikipedia.org/wiki/Hohmann_transfer_orbit</ref> is an elliptical orbit used to transfer between two circular orbits of different radii in the same plane. In general a Hohmann transfer orbit uses the lowest possible amount of energy in traveling between two objects orbiting at these radii, and so is used to send the maximum amount of mission payload with the fixed amount of energy that can be imparted by a particular rocket. Non-Hohmann transfer paths may have other advantages for a particular mission such as shorter transfer times, but will necessarily require a reduction in payload mass and/or use of a more powerful rocket. | ||
| − | == Forced orbit == | + | ==Forced orbit== |
A forced orbit is any powered orbit that depends on a vehicle engine or aerobraking to achieve orbital transfer between two bodies. | A forced orbit is any powered orbit that depends on a vehicle engine or aerobraking to achieve orbital transfer between two bodies. | ||
Revision as of 13:30, 19 April 2019
Orbit is the trajectory of an object moving in a circular, elliptical, or hyperbolic path around a bigger object, attracted by its gravity. Mars and other planets are orbiting the Sun in an elliptical trajectory. Mars is orbited by two moons: Phobos and Deimos.
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LEO
Low Earth Orbit is the minimum height (160 km) and velocity (8 km/s) that an object needs to stay in orbit round Earth. This orbit is the easiest to reach with currently available rocketry. It might be used to assemble a large spaceship from smaller parts that are lifted separately from Earth. LEO is subject to drag from the Earth's atmosphere and vehicles in LEO need to be booster periodically to avoid orbital decay and re-entry.
LMO
Low Mars orbit. Effect of Mars shape. Effect of Mars atmosphere.
Hohmann transfer orbit
In orbital mechanics, the Hohmann transfer orbit[1] is an elliptical orbit used to transfer between two circular orbits of different radii in the same plane. In general a Hohmann transfer orbit uses the lowest possible amount of energy in traveling between two objects orbiting at these radii, and so is used to send the maximum amount of mission payload with the fixed amount of energy that can be imparted by a particular rocket. Non-Hohmann transfer paths may have other advantages for a particular mission such as shorter transfer times, but will necessarily require a reduction in payload mass and/or use of a more powerful rocket.
Forced orbit
A forced orbit is any powered orbit that depends on a vehicle engine or aerobraking to achieve orbital transfer between two bodies.
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