Editing Starwisp

{{short description|1985 proposal for microwave sail flyby of a nearby star}}
'''Starwisp''' is a hypothetical unmanned [[interstellar probe]] design proposed by the late [[Robert L. Forward]]. It is propelled by a [[microwave]] sail, similar to a [[solar sail]] in concept, but powered by microwaves from a human-made source. It would fly through the target system without slowing down.

== Description ==

"Starwisp" is a concept for an ultra-low-mass interstellar probe pushed by a microwave beam. It was proposed by scientist and author [[Robert L. Forward]] in 1985,<ref name="Forward1985">{{cite journal| title=Starwisp: an Ultralight Interstellar Probe| journal=American Institute of Aeronautics and Astronautics Journal of Spacecraft and Rockets| volume=22|date=May–June 1985| first=Robert| last=Forward|authorlink=Robert L. Forward}}</ref> and further work was published by [[Geoffrey A. Landis]] in 2000.<ref name="Landis2000">Landis, Geoffrey A. "Microwave Pushed Interstellar Sail: Starwisp Revisited" (paper AIAA-2000-3337, presented at the [[AIAA]] 36th Joint Propulsion Conference and Exhibit, Huntsville AL, July 17–19, 2000).</ref> The proposed device uses [[beam-powered propulsion]] in the form of a high-power microwave [[Antenna (radio)|antenna]] pushing a sail. The probe itself would consist of a mesh of extremely fine carbon wires about 100&nbsp;m across, with the wires spaced the same distance apart as the 3&nbsp;mm [[wavelength]] of the microwaves that will be used to push it.

Forward proposed that the wires would incorporate [[Nanoscopic scale|nanoscale]] computer circuitry, sensors, microwave power collection systems and microwave [[Transmitter|radio transmitters]] fabricated on the wire surfaces, giving the probe data collection and transmission capability. Being distributed across the entire sail, no "rigging" is needed, as would be the case if the mission electronics were placed in a separate probe that was pulled by the sail.

The original Starwisp concept assumed that the microwaves would be efficiently reflected, with the wire mesh surface acting as a [[superconductor]] and nearly perfectly efficient mirror. This assumption is not valid. Landis showed that a grid will absorb a significant fraction of the power incident on it, and therefore cannot stay cool enough to be [[Superconductivity|superconducting]]. The design is thermally limited, hence the use of carbon as the material in Landis's concept. 

Low mass was the key feature of the Starwisp probe. In Landis's calculations, the mesh has a density of only 100&nbsp;kg/km<sup>2</sup>, for a total mass of 1&nbsp;kg, plus a payload of 80&nbsp;grams.

Although the [[Beam divergence|diffraction limit]] severely constrains the range of the transmitting antenna, the probe is designed to have an acceleration of 24&nbsp;m/s<sup>2</sup>, so that it can reach a significant fraction of the speed of light within a very short distance, before passing out of range. The antenna uses a microwave lens 560&nbsp;km in diameter, would transmit 56&nbsp;GW of power, and would accelerate the probe to 10% of the speed of light.

The probe would cruise without power for decades until it finally approached the target [[star]], at which point the antenna which launched it would again target its beam on Starwisp. This would be done when the Starwisp was about 80% of the way to its destination, so that the beam and Starwisp would arrive there at the same time. At such extreme long range the antenna would be unable to provide any propulsion, but Starwisp would be able to use its wire sail to collect and convert some of the [[Microwave power transmission|microwave energy into electricity]] to operate its sensors and transmit the data it collects back home. Starwisp would not slow down at the target star, performing a high-speed flyby mission instead.

Since the antenna is only required for a few days at Starwisp's launch and again for another few days several decades later to power it while it passes its target, Starwisp probes might be mass-produced and launched by the maser every few days. In this manner, a continuous stream of data could be collected about distant solar systems even though any given Starwisp probe only spends a few days travelling through it. Alternatively, the launching transmitter could be used in the interim to transmit power to Earth for commercial use, as with a [[solar power satellite]].

==Possible methods of fabrication==
Constructing such a delicate probe would be a significant challenge. One proposed method would be to "paint" the probe and its circuitry onto an enormous sheet of plastic which degrades when exposed to [[ultraviolet]] light, and then wait for the sheet to evaporate away under the assault of solar UV after it has been deployed in space.

Another proposed method noted that the Starwisp probe wires were of the same physical scale as wires and circuit elements on modern [[Integrated circuit|computer microchips]] and could be produced by the same [[Photolithography|photolithographic fabrication technologies]] as those of computer chips. The probe would have to be built in sections the size of current chip fabrication silicon wafers and then connected together.

== Technical problems ==

A major problem this design would face would be the radiation encountered en route. Travelling at 20% of [[Speed of light|light speed]], ordinary interstellar hydrogen would become a significant radiation hazard, and the Starwisp would be without shielding and likely without active self-repair capability. Another problem would be keeping the acceleration of the Starwisp uniform enough across its sail area so that its delicate wires would not tear or be twisted out of shape. Distorting the shape of the Starwisp even slightly could result in a runaway catastrophe, since one portion of the Starwisp would be reflecting microwaves in a different direction than the other portion and be thrust even farther out of shape. Such delicate and finely-balanced control may prove impossible to realize.

The possibility of using a [[dusty plasma]] sail{{fact|date=July 2018}} in which a dusty substance that is maintained as a plasma within space is responsible for the reflection of electromagnetic radiation could circumvent problems associated with radiation damage to the medium responsible for the transfer of [[radiation pressure]] (the dusty plasma sail might not be as easy to damage as a thin film or the like). Dusty plasma sails can also adapt their three-dimensional structure in real time to ensure reflection perpendicular to any incident light/microwave beam.

==In fiction==
*In a [[science fiction]] story Forward suggested that the beam from a solar power satellite could be used to push a Starwisp probe while the solar power satellite was being tested after construction.<ref name="Forward1990">{{cite journal| title=Fade to Black| first=Robert| last=Forward| authorlink=Robert L. Forward|journal=[[Analog Science Fiction and Fact|Analog]]|date=December 1990}}</ref>

== See also ==
* [[Breakthrough Starshot]], a funded proposal for laser-propelled Starwisp-type spacecraft

== References ==
{{reflist}}

==External links==
* [http://ffden-2.phys.uaf.edu/213.web.stuff/Scott%20Kircher/lightsails.html Light Sails]
* [http://www.aleph.se/Trans/Tech/Space/laser.txt Small Laser-propelled Interstellar Probe]
* [https://web.archive.org/web/20091213185941/http://science.nasa.gov/newhome/headlines/prop08apr99_1.htm Setting Sail for the Stars]
* [http://www.transorbital.net/Library/D001_AxA.html Beamed Power Propulsion To The Stars] {{Webarchive|url=https://web.archive.org/web/20171106175011/http://www.transorbital.net/Library/D001_AxA.html |date=2017-11-06 }}

[[Category:Hypothetical spacecraft]]
[[Category:Interstellar travel]]
[[Category:1985 in science]]