A cycler is a potential spacecraft on a closed transfer orbit that would pass close to two celestial bodies at regular intervals. Cyclers could be used for carrying heavy supplies, life support and radiation shielding.
Concept
editA cycler encounters two or more bodies regularly by employing a free-return trajectory, this trajectory was analysed by Arthur Schwaniger in 1963 with a symmetrical orbit past the Moon and Earth.[1] Once the orbit is established, no propulsion is required to shuttle between the two, although some minor corrections may be necessary due to small perturbations in the orbit. The use of cyclers was considered in 1969 by Walter M. Hollister, who examined the case of an Earth–Venus cycler.[2] Hollister did not have any particular mission in mind, but posited their use for both regular communication between two planets, and for multi-planet flyby missions.[3]
Triple cycler
editAn extension of a cycler is the triple cycler like an Earth-Venus-Mars cycler,[4] or a Jovian system moon to moon cycler.[5]
Types of cyclers by purpose
editVenus cycler
editWalter M. Hollister considered in 1969 the concept of a cycler and examined the case of an Earth–Venus cycler.[2]
Lunar cycler
editA lunar cycler or Earth–Moon cycler is a cycler orbit, or spacecraft therein, which periodically passes close by the Earth and the Moon, using gravity assists and occasional propellant-powered corrections to maintain its trajectories between the two. If the fuel required to reach a particular cycler orbit from both the Earth and the Moon is modest, and the travel time between the two along the cycler is reasonable, then having a spacecraft in the cycler can provide an efficient and regular method for space transportation.[6]
Mars cycler
editA Mars cycler or Earth–Mars cycler is a spacecraft trajectory that encounters the Earth and Mars on a regular basis, or a spacecraft on such a trajectory
Interstellar cycler
editAn interstellar cycler or Schroeder cycler, a theoretical spacecraft trajectory that encounters two or more stars on a regular basis, or a spacecraft on such a trajectory.
An interstellar cycler would never slow down and use Lorentz force for turning. The envisioned benefit is that the life support for an interstellar vehicle wouldn't have to be accelerated, only the payload, allowing more to be carried for a given energy budget.
As an idea it was considered by P.C. Norem in a 1969 paper[7] and popularized by Karl Schroeder in his 2002 novel Permanence.
References
edit- ^ Schwaninger, Arthur J. (1963). Trajectories in the Earth-Moon Space with Symmetrical Free Return Properties. Technical Note D-1833. Huntsville, Alabama: NASA / Marshall Space Flight Center.
- ^ a b Hollister 1969, p. 366.
- ^ Hollister 1969, p. 369.
- ^ Jones, Drew R; Hernandez, Sonia; Jesick, Mark (August 24, 2017). "(PDF) Low Excess Speed Triple Cyclers of Venus, Earth, and Mars". ResearchGate. Retrieved October 14, 2024.
- ^ Hernandez, Sonia; Jones, Drew R; Jesick, Mark (August 1, 2017). "(PDF) One Class of Io-Europa-Ganymede Triple Cyclers". ResearchGate. Retrieved October 14, 2024.
- ^ Kenneth D. Mease; Benjamin F. Villac; Josep M. Mondelo; et al. (Jordi Casoliva Rodon) (June 2008). Economical Space Transportation Routes Between Earth, Moon, and Beyond (PDF) (Report). University of California. p. 2. Archived from the original (PDF) on 2014-09-08.
- ^ Interstellar Travel: A Round Trip Propulsion System with Relativistic Velocity Capabilities,” AAS paper 69-388 (June, 1969).
Additional references
edit- Hollister, W. M. (1969). "Periodic orbits for interplanetary flight". Journal of Spacecraft and Rockets. 6 (4): 366–369. Bibcode:1969JSpRo...6..366H. doi:10.2514/3.29664. ISSN 0022-4650. }
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