Stellar engine

(Redirected from Shkadov thruster)

Stellar engines are a class of hypothetical megastructures which use the resources of a star to generate available work (also called exergy). For instance, they can use the energy of the star to produce mechanical, electrical or chemical work or they can use the impulse of the light emitted by the star to produce thrust, able to control the motion of a star system.[1] The concept has been introduced by Bădescu and Cathcart.[2] The variants which produce thrust may accelerate a star and anything orbiting it in a given direction.[3][4] The creation of such a system would make its builders a type-II civilization on the Kardashev scale.

Diagram of a class-C stellar engine (to scale) built around a Sun-like star. It consists of a partial Dyson swarm composed of 5 Dyson rings of solar collectors (the class-B component), and a large statite Shkadov thruster (the class-A component). Perspective is from below the system's ecliptic at a distance of ~2.8 AU. The system's direction of acceleration is on a vector from the center of the star through the center of the Shkadov thruster, which is hovering over the star's north pole (with regards to the ecliptic), at a distance of 1 AU.

Classes

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Three classes of stellar engines have been defined.[2]

Class A (Shkadov thruster)

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One of the simplest examples of a stellar engine is the Shkadov thruster (named after Dr. Leonid Shkadov, who first proposed it), or a class-A stellar engine.[5] Such an engine is a stellar propulsion system, consisting of an enormous mirror/light sail—actually a massive type of solar statite large enough to classify as a megastructure—which would balance gravitational attraction towards and radiation pressure away from the star. Since the radiation pressure of the star would now be asymmetrical, i.e. more radiation being emitted in one direction as compared to another, the "excess" radiation pressure acts as net thrust, accelerating the star in the direction of the hovering statite. Such thrust and acceleration would be very slight, but such a system could be stable for millennia. Any planetary system attached to the star would be "dragged" along by its parent star. For a star such as the Sun, with luminosity 3.85×1026 W and mass 1.99×1030 kg, the total thrust produced by reflecting half of the solar output would be 1.28×1018 N. After a period of one million years this would yield an imparted speed of 20 m/s, with a displacement from the original position of 0.03 light-years. After one billion years, the speed would be 20 km/s and the displacement 34,000 light-years, a little over a third of the estimated width of the Milky Way galaxy.

Class B

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A class-B stellar engine consists of two concentric spheres around a star. The inner sphere (which may be assimilated with a Dyson shell) receives energy from the star and becomes hotter than the outer sphere. The difference of temperature between the two spheres drives thermal engines able to provide mechanical work.

Unlike the Shkadov thruster, a class-B stellar engine is not propulsive.

Class C

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A class-C stellar engine, such as the Badescu–Cathcart engine,[2] combines the two other classes, employing both the propulsive aspects of the Shkadov thruster and the energy generating aspects of a class-B engine. A higher temperature Dyson shell partially covered by a mirror combined with an outer sphere at a lower temperature would be one incarnation of such a system. The non-spherical mirror ensures conversion of light impulse into effective thrust (like a class-A stellar engine) while the difference of temperature may be used to convert star energy into mechanical work (like a class-B stellar engine). Notice that such system suffers from the same stabilization problems as a non-propulsive shell, as would be a Dyson swarm with a large statite mirror (see image above). A Dyson bubble variant is already a Shkadov thruster (provided that the arrangement of statite components is asymmetrical); adding energy extraction capability to the components seems an almost trivial extension.

Caplan thruster

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Astronomer Matthew E. Caplan of Illinois State University has proposed a type of stellar engine that uses concentrated stellar energy (repurposing the mirror statites from class A) to excite certain regions of the outer surface of the star and create beams of solar wind for collection by a multi-Bussard ramjet assembly. The ramjets would produce directed plasma to stabilize its orbit and jets of oxygen-14 to push the star. Using rudimentary calculations that assume maximum efficiency, Caplan estimates that the Bussard engine would use 1012 kg of solar material per second to produce a maximum acceleration of 10−9 m/s2, yielding a velocity of 200 km/s after 5 million years and a distance of 10 parsecs over 1 million years. While theoretically the Bussard engine would work for 100 million years, given the mass loss rate of the Sun, Caplan deems 10 million years to be sufficient for a stellar collision avoidance.[6] His proposal was commissioned by the German educational YouTube channel Kurzgesagt.[7]

Svoronos Star Tug

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Alexander A. Svoronos of Yale University proposed the 'Star Tug', a concept that combines aspects of the Shkadov thruster and Caplan engine to produce an even more powerful and efficient mechanism for controlling a star's movement. Essentially, it replaces the giant parabolic mirror of the Shkadov thruster with an engine powered by mass lifted from the star, similar to the Caplan engine. However, instead of pushing a star from behind with a beam of thrust, as the Caplan engine does, it pulls the star from the front via its gravitational link to it, same as the Shkadov thruster. As a result, it only needs to produce a single beam of thrust (toward but narrowly missing the star), whereas the Caplan engine must produce two beams of thrust (one to push the star from behind and negate the force of gravity between the engine and the star, and one to propel the system as a whole forward). The result is that the Svoronos Star Tug is a much more efficient engine capable of significantly higher accelerations and max velocities. The Svoronos Star Tug can, in principle (assuming perfect efficiency), accelerate the Sun to ~27% the speed of light (after burning enough of the Sun's mass to transition it to a brown dwarf).[8]

See also

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References

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  1. ^ "Stellar_Engines.pdf". Google Docs. Retrieved 2022-06-12.
  2. ^ a b c Badescu, Viorel; Cathcart, Richard B. (2000). "Stellar engines for Kardashev's Type II Civilization". Journal of the British Interplanetary Society. 53: 297–306. Bibcode:2000JBIS...53..297B. Archived from the original on 2018-08-24. Retrieved 2013-07-01.
  3. ^ Badescu, Viorel; Cathcart, Richard B. (February 2006). "Use of Class A and Class C stellar engines to control Sun movement in the galaxy". Acta Astronautica. 58 (3): 119–129. Bibcode:2006AcAau..58..119B. doi:10.1016/j.actaastro.2005.09.005.
  4. ^ Badescu, Viorel; Cathcart, Richard B. (2006). "Chapter 12: Stellar Engines and the Controlled Movement of the Sun". Macro-Engineering: A Challenge for the Future. Water Science and Technology Library. Vol. 54. pp. 251–280. doi:10.1007/1-4020-4604-9_12. ISBN 978-1-4020-3739-9.
  5. ^ Shkadov, Leonid (10–17 October 1987). "Possibility of controlling solar system motion in the Galaxy". Proceedings of the IAF 38th International Astronautical Congress. 38th International Astronautical Congress IAC 1987. Brighton, England: International Astronautical Federation. pp. 1–8. Bibcode:1987brig.iafcR....S.
  6. ^ Caplan, Matthew (December 17, 2019). "Stellar engines: Design considerations for maximizing acceleration". Acta Astronautica. 165: 96–104. Bibcode:2019AcAau.165...96C. doi:10.1016/j.actaastro.2019.08.027. S2CID 203111659. Archived from the original on December 23, 2019. Retrieved December 22, 2019.
  7. ^ "How to Move the Sun: Stellar Engines". YouTube. Kurzgesagt. December 22, 2019. Archived from the original on 2021-12-21. Retrieved April 26, 2021.
  8. ^ Svoronos, Alexander A. (2020-11-01). "The Star Tug: An active stellar engine capable of accelerating a star to relativistic velocities". Acta Astronautica. 176: 306–312. Bibcode:2020AcAau.176..306S. doi:10.1016/j.actaastro.2020.07.005. ISSN 0094-5765. S2CID 224962621.