A statite (a portmanteau of the words static and satellite) is a hypothetical type of artificial satellite that employs a solar sail to continuously modify its orbit in ways that gravity alone would not allow. Typically, a statite would use the solar sail to "hover" in a location that would not otherwise be available as a stable geosynchronous orbit. Statites have been proposed that would remain in fixed locations high over Earth's poles, using reflected sunlight to counteract the gravity pulling them down. Statites might also employ their sails to change the shape or velocity of more conventional orbits, depending upon the purpose of the particular statite.
The concept of the statite was invented independently and at about the same time by Robert L. Forward[1] (who coined the term "statite") and Colin McInnes, who used the term "halo orbit"[2] (not to be confused with the type of halo orbit discovered by Robert Farquhar). Subsequently, the terms "non-Keplerian orbit" and "artificial Lagrange point" have been used as a generalization of the above terms.
No statites have been deployed to date, as solar sail technology remains in its infancy. NASA's cancelled Sunjammer solar sail mission had the stated objective of flying to an artificial Lagrange point near the Earth/Sun L1 point, to demonstrate the feasibility of the Geostorm[3]geomagnetic storm warning mission concept proposed by NOAA's Patricia Mulligan.[4] A constellation of statites has been proposed for performing a rendezvous with an interstellar object.[5]
A so-called quasite is a variation of a statite, being slightly unbalanced to allow other forces to balance its position, though having a slow orbit. This is employed in the proposal by David Kipping for a so-called Torqued Accelerator using Radiation from the Sun (TARS) slingshot accelerator,[6] essentially being a light mill in space.[7]
See also
References
- ↑ Patente estadounidense 5183225 , Robert L. Forward & Forward, "Statite: Nave espacial que utiliza presión de luz y método de uso", emitida el 2 de febrero de 1993.
- ↑ McInnes, CR y Simmons, JFL: "Órbitas de halo para velas solares: dinámica y aplicaciones", ESA Journal , vol. 13, 1989, págs. 229-234
- ↑ Geotormenta
- ↑ Mulligan, Patricia (agosto de 1998). "Velas solares para la comunidad espacial operativa". Spaceviews . 8 ( 3–4 ).
- ↑ Cody, Sara (6 de mayo de 2020). "Para atrapar a un visitante interestelar, use una catapulta espacial alimentada por energía solar" . Noticias del MIT, Departamento de Aeronáutica y Astronáutica . Recuperado el 6 de enero de 2025 .
- ↑ Cooper, Keith (8 de septiembre de 2025). "Un lanzador espacial que lleva el nombre de un robot de 'Interstellar' podría ayudarnos a llegar a otro sistema estelar. Aquí te contamos cómo" . Space . Consultado el 28 de noviembre de 2025 .
- ↑ Kipping, David; Lampo, Kathryn (2025). "Acelerador de torsión que utiliza radiación del Sol (TARS) para cargas útiles interestelares". arXiv : 2507.17615v1 [ physics.space-ph ].
- Astrodinámica
- Tecnología hipotética
- Conceptos de vuelos espaciales
- restos de naves espaciales