Engineering:Whipple shield
The Whipple shield or Whipple bumper, invented by Fred Whipple,[1] is a type of spaced armor shielding to protect crewed and uncrewed spacecraft from hypervelocity impact / collisions with micrometeoroids and orbital debris whose velocities generally range between 3 and 18 kilometres per second (1.9 and 11.2 mi/s). According to NASA, the Whipple shield is designed to withstand collisions with debris up to 1 cm, which helps to mitigate the Kessler syndrome.[2]
Shield
In contrast to monolithic shielding of early spacecraft, Whipple shields consist of a relatively thin outer bumper spaced some distance from the main spacecraft wall. The bumper is not expected to stop the incoming particle or even remove much of its energy, but to break up and disperse it, dividing the original particle energy among many fragments that fan out between bumper and wall. The original particle energy is spread more thinly over a larger wall area, which is more likely to withstand it. Although a Whipple shield lowers total spacecraft mass compared to a solid shield (always desirable in spaceflight), the extra enclosed volume may require a larger payload fairing.
There are several variations on the simple Whipple shield. Multi-shock shields,[3][4] like the one used on the Stardust spacecraft, use multiple bumpers spaced apart to increase the shield's ability to protect the spacecraft. Whipple shields that have a filling in between the rigid layers of the shield are called stuffed Whipple shields.[5][6] The filling in these shields is usually a high-strength material like Kevlar or Nextel aluminium oxide fiber.[7] The type of shield, the material, thickness and distance between layers are varied to produce a shield with minimal mass that will also minimize the probability of penetration. There are over 100 shield configurations on the International Space Station alone,[8] with important and high-risk areas having better shielding.
See also
- Micrometeoroid shielding
- Spaced armor
- Double hull
References
- ↑ Whipple, Fred L. (1947), "Meteorites and Space Travel", Astronomical Journal 52: 131, doi:10.1086/106009, Bibcode: 1947AJ.....52Q.131W
- ↑ "STARDUST Whipple Shield". https://solarsystem.nasa.gov/stardust/spacecraft/whipple.html.
- ↑ Cour-Palais, Burton G.; Crews, Jeanne L. (1990), "A Multi-Shock Concept for Spacecraft Shielding", International Journal of Impact Engineering 10 (1–4): 135–146, doi:10.1016/0734-743X(90)90054-Y
- ↑ Crews, Jeanne L. & Burton G. Cour-Palais, "Hypervelocity Impact Shield", US patent 5067388, issued November 26, 1991
- ↑ Christiansen, Eric L.; Crews, Jeanne L.; Williamsen, Joel E.; Robinson, Jennifer H.; Nolen, Angela M. (1995), "Enhanced Meteoroid and Orbital Debris Shielding", International Journal of Impact Engineering 17 (1–3): 217–228, doi:10.1016/0734-743X(95)99848-L, https://zenodo.org/record/1258555
- ↑ Crews, Jeanne L.; Eric L. Christiansen & Jennifer H. Robinson et al., "Enhanced Whipple Shield", US patent 5610363, issued March 11, 1997
- ↑ 3M Nextel Ceramic Fabric Offers Space Age Protection, 3M Company, http://www.3m.com/market/industrial/ceramics/pdfs/CeramicFabric.pdf, retrieved September 4, 2011
- ↑ Christiansen, Eric L. (2003) (Technical Report), Meteoroid/Debris Shielding, Washington DC: National Aeronautics and Space Administration, p. 13, TP−2003-210788, archived from the original on 2013-02-25, https://web.archive.org/web/20130225001045/http://ston.jsc.nasa.gov/collections/TRS/_techrep/TP-2003-210788.pdf
External links
- Brief descriptions of spacecraft shielding by NASA
- B.G. Cour-Palais' reminisces of the Apollo meteoroid protection program
- The Skylab meteoroid shield design and development
- ESA Giotto dust shield
- J.L. Crews' recounting of the invention of the multi-shock shield, pp. 21–29
- Installing the Nextel/Kevlar blankets in the Destiny laboratory stuffed Whipple Shields
- Meteoroid/Debris Protection System Development at ESA for ATV and Columbus
- Hyper-velocity impact test at JAXA of Kibo's debris shield
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