Difference between revisions of "Low energy trajectories"
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Cargo could be inserted into '''low-energy trajectories'''. These trajectories will take longer then current [[Hohmann transfer|Hohmann transfer orbits]], but will save [[propellant]] and thus allow more payload. | Cargo could be inserted into '''low-energy trajectories'''. These trajectories will take longer then current [[Hohmann transfer|Hohmann transfer orbits]], but will save [[propellant]] and thus allow more payload. | ||
Low cost of transport will be vital in [[Unmanned setup of a whole settlement|setting up a colony]] and in resupplying a [[semi-autonomous colony]]. It also allows for some items to be tradable without a tremendous transportation cost. | Low cost of transport will be vital in [[Unmanned setup of a whole settlement|setting up a colony]] and in resupplying a [[semi-autonomous colony]]. It also allows for some items to be tradable without a tremendous transportation cost. | ||
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==Methods== | ==Methods== | ||
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*The [https://en.wikipedia.org/wiki/Interplanetary_Transport_Network Interplanetary Transport Network] | *The [https://en.wikipedia.org/wiki/Interplanetary_Transport_Network Interplanetary Transport Network] | ||
*Using [[ion thrusters]]/[[solar sails]]/[[plasma sails]] | *Using [[ion thrusters]]/[[solar sails]]/[[plasma sails]] | ||
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==Disadvantages== | ==Disadvantages== | ||
| − | *Such trajectories will take much longer then Hohmann transfers | + | *Such trajectories will take much longer then Hohmann transfers. Thus it is not suitable for time sensitive cargo. |
| − | *Low energy transfer orbits can only launch when Mars and Earth are in the correct orbital positions. Where as high energy trajectories can launch in larger time windows | + | *This means cargo will be exposed to the harsh conditions of space for a longer period of time. This may limit what types of cargo are suitable for these paths. |
| − | + | *Low energy transfer orbits can only launch when Mars and Earth are in the correct orbital positions. Where as high energy trajectories can launch more often, in larger time windows. | |
[[category:Orbital Mechanics]] | [[category:Orbital Mechanics]] | ||
Latest revision as of 04:49, 21 November 2022
Cargo could be inserted into low-energy trajectories. These trajectories will take longer then current Hohmann transfer orbits, but will save propellant and thus allow more payload. Low cost of transport will be vital in setting up a colony and in resupplying a semi-autonomous colony. It also allows for some items to be tradable without a tremendous transportation cost.
Methods
- Bi-elliptic transfers
- The Interplanetary Transport Network
- Using ion thrusters/solar sails/plasma sails
Disadvantages
- Such trajectories will take much longer then Hohmann transfers. Thus it is not suitable for time sensitive cargo.
- This means cargo will be exposed to the harsh conditions of space for a longer period of time. This may limit what types of cargo are suitable for these paths.
- Low energy transfer orbits can only launch when Mars and Earth are in the correct orbital positions. Where as high energy trajectories can launch more often, in larger time windows.
