Difference between revisions of "Mars cycler"

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A Mars cycler is a hypothetical [[Mission concepts|transportation]] system between Earth and Mars.
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A Mars cycler, as described in <ref>https://youtu.be/42Je9Xczu0o?t=653</ref>, is a hypothetical [[Mission concepts|transportation]] system between Earth and Mars proposed by Buzz Aldrin as a way to reach Mars more economically.<ref>Wikipedia Mars Cycler https://en.wikipedia.org/wiki/Mars_cycler</ref>.
  
The cycler is a vehicle on an elliptical orbit the crosses both the Earth's and Mars' orbit.  This allows it periodically to be reached by a shuttle, either from Earth of from Mars. While moving with the cycler, no energy is expended by the shuttle. The cycler can serve as an habitat, and in particular provide radiation protection from relatively heavy construction, compared to the shuttles.
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It is a vehicle on an elliptical orbit the crosses both the Earth's and Mars' orbits with transit times of about 5 month in either direction.  This allows it periodically to be reached by a shuttle, either from Earth of from Mars. While moving with the cycler, no energy is expended by the shuttle. The cycler can serve as a more hospitable habitat than the shuttles: in particular it can provide better radiation protection from relatively heavy construction, artificial spin gravity and larger amounts of electricity for its [https://en.wiktionary.org/wiki/hotel_load hotel load].
  
The shuttles require about 6000 m/s to reach the cycler from Earth and another 9700 m/s to slow down when they reach Mars. However, the deltaV at Mars could be replaced by aerodynamic capture, saving on propellant.  On the reverse leg of the journey, the deltav requirements would be similar.
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The shuttles require about 6km/s of [[Propulsion#Velocity_.28Rocket_equation.29|deltaV]] to reach the cycler from Earth and another 9.7km/s to slow down when they reach Mars, possibly reduced with the aid of [[skyhook|skyhooks]] or the use of aerodynamic capture.  On the reverse leg of the journey, the [[Propulsion#Velocity_.28Rocket_equation.29|deltaV]] requirements would be similar.
  
The transit times between the two planets would be about 5 month in either direction.
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An alternate approach would involve the cycler with a more efficient but generally mass or energy prohibitive thruster such as a [[Nuclear_thermal_propulsion|nuclear thermal]], [[Ion_thruster#Pulsed_Fission_Fusion_.28PuFF.29|Pulsed Fission Fusion(PuFF)]] or [[Ion_thruster#VASIMR|VASIMR]] thruster. This may reduce the [[Propulsion#Velocity_.28Rocket_equation.29|deltaV]] requirements for the comparably lower efficiency shuttle engines, increasing the effective mass fraction or decreasing trip time.
 
 
The Mars cycler was proposed by Buzz Aldrin as a way to reach Mars more economically.<ref>Wikipedi Mars Cycler https://en.wikipedia.org/wiki/Mars_cycler</ref>
 
  
 
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==References==
 
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Revision as of 06:11, 11 November 2020

A Mars cycler, as described in [1], is a hypothetical transportation system between Earth and Mars proposed by Buzz Aldrin as a way to reach Mars more economically.[2].

It is a vehicle on an elliptical orbit the crosses both the Earth's and Mars' orbits with transit times of about 5 month in either direction. This allows it periodically to be reached by a shuttle, either from Earth of from Mars. While moving with the cycler, no energy is expended by the shuttle. The cycler can serve as a more hospitable habitat than the shuttles: in particular it can provide better radiation protection from relatively heavy construction, artificial spin gravity and larger amounts of electricity for its hotel load.

The shuttles require about 6km/s of deltaV to reach the cycler from Earth and another 9.7km/s to slow down when they reach Mars, possibly reduced with the aid of skyhooks or the use of aerodynamic capture. On the reverse leg of the journey, the deltaV requirements would be similar.

An alternate approach would involve the cycler with a more efficient but generally mass or energy prohibitive thruster such as a nuclear thermal, Pulsed Fission Fusion(PuFF) or VASIMR thruster. This may reduce the deltaV requirements for the comparably lower efficiency shuttle engines, increasing the effective mass fraction or decreasing trip time.

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References