James Webb Space Telescope sunshield
![]() | This article may require cleanup to meet Wikipedia's quality standards. The specific problem is: poorly written. (December 2021) |
![](http://upload.wikimedia.org/wikipedia/commons/thumb/6/6f/James_Webb_Space_Telescope_2009_bottom.jpg/220px-James_Webb_Space_Telescope_2009_bottom.jpg)
The James Webb Space Telescope (JWST) sunshield is a passive thermal control system deployed post-launch to shield the telescope and instrumentation from the light and heat of the Sun, Earth, and Moon. Its purpose is to enable the infrared telescope to function at or below its design temperature of 40 kelvins (−233 °C; −388 °F). Its intricate deployment was successfully completed on January 4, 2022, ten days after launch when it was more than 0.8 million kilometers (500,000 mi) away from Earth.[1][2]
The JWST sunshield was folded up to fit within the fairing of the launch rocket and was deployed post-launch, unfolding a large metal-coated sheet of material. The material is designed to shield the main optics from the Sun's light and heat, so the telescope can see the faint light coming from distant stars and galaxies. The sunshield segment includes the layers and its deployment mechanisms, which also includes the trim flap.[3][4]
The layers of the sunshield provide insulation for the optics and help dissipate heat. The shield has five layers, and each layer is roughly the size of a tennis court. Each layer is as thin as a human hair and is made of a Kapton membrane coated with aluminum for reflectivity. The purple color of the outermost Sun-facing layers comes from the doped-silicon coating (the same material used in computer chips) which toughens the shield and helps it reflect heat.[5] The thickness of the aluminum coating is approximately 100 nanometers, and the silicon coating is even thinner at approximately 50 nanometers.[6] The telescope uses the sunshield to stop itself from being heated up by infrared radiation from the Sun and other nearby planetary objects, which would otherwise inhibit normal operations of onboard instruments.
Overview[]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/5/56/James_Webb_Space_Telescope_%2814742910940%29.jpg/220px-James_Webb_Space_Telescope_%2814742910940%29.jpg)
To make observations in the near and mid infrared spectrum, the JWST must be kept very cold (under 40 K (−233 °C; −388 °F)), otherwise infrared radiation from the telescope itself would overwhelm its instruments. Therefore, it uses a large sunshield to block light and heat from the Sun, Earth, and Moon, and its position near the Sun-Earth L2 Lagrange point keeps all three bodies on the same side of the spacecraft at all times.[7] Its halo orbit around L2 avoids the shadow of the Earth and Moon, maintaining a constant environment for the sunshield and solar arrays.[8]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/e/e6/Folded_sun_umbrella_%288287862593%29.jpg/220px-Folded_sun_umbrella_%288287862593%29.jpg)
Infrared is heat radiation. In order to see the faint glow of infrared heat from distant stars and galaxies, the telescope has to be very cold. If the telescope were heated by sunlight or the warm glow of the Earth, the infrared light emitted by the telescope would outshine its targets, and it wouldn’t be able to see anything.
— NASA Deputy Senior Project Scientist for the Webb Telescope at Goddard, 2008[10]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/1/1c/The_hot_and_code_sides_of_the_JWST_sunshield.jpg/220px-The_hot_and_code_sides_of_the_JWST_sunshield.jpg)
The sunshield acts as large parasol allowing the main mirror, optics, and instruments to passively cool to 40 kelvins (−233 °C; −388 °F) or lower.[4] The kite-shaped sunshield is about 22 by 10 metres (72 by 33 ft) in size.[11] It is big enough to shade the main mirror and secondary mirror, leaving only one instrument, the MIRI (Mid-Infrared Instrument), in need of extra cooling.[4] The sunshield acts as a and causes a temperature drop of 318 K (318 °C, 604 °F)[12] from front to back.[11] The telescope needs to be colder than the objects it is attempting to observe.[13] It needs to be cold enough that its internal infrared emissions are significantly less than the observed objects at the relevant wavelengths. The sunshield is a critical part of the telescope to achieve temperatures low enough for the sensitive infrared observations it is planning to make.[13] The sunshield membrane is one of the enabling technologies that will allow the JWST to operate.[14]
The sunshield has five layers to mitigate the conduction of heat.[4] The five layers are made of the polyimide film Kapton E, which is stable at very low temperatures.[4] The Kapton film is coated with aluminum, and the Sun-facing sides of the outermost two layers are also coated with silicon treated or "doped" with other elements.[4][5] This helps the material survive in space, radiate excess heat, and to conduct electricity so a static charge does not build up on the layers.[4] Kapton is noted for being stable from −269 to 400 °C (−450 to 750 °F).[5] However, in the long term, even in Earth storage conditions, Kapton can eventually degrade; Kapton used on the Skylab Apollo Telescope Mount had degraded after 40 years.[15] Accidental tears of the delicate film structure during testing in 2018 were among the factors delaying the JWST project.[16]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/d/d9/James_Webb_telescope_sunshield.jpg/220px-James_Webb_telescope_sunshield.jpg)
Each layer has a slightly different shape and size.[4] The level 5 layer is the closest to the primary mirror and is the smallest. The layer closest to the Sun is called layer 1 and is bigger and flatter.[4] The first layer blocks 90% of the heat, and each successive layer blocks more heat, which is reflected out the sides.[4][13] The sunshield allows the optics to stay in shadow for pitch angles of +5° to −45° and roll angles of +5° to −5°.[14] The layers are designed with Thermal Spot Bond (TSB), which helps stop a rip or hole from increasing in size should one occur.[4] There is a grid pattern bonded to each layer at intervals.[4] The first layer is .05 mm (0.002 in) thick, and the other layers are .025 mm (0.001 in) thick.[5] The doped-silicon layer is 50 nanometers (nm) thick.[5] A 100 nm thick aluminum coating is applied to the front and back of all five layers.[5] In operation the shield will receive about 200 kilowatts of solar radiation, but only pass 23 milliwatts to the other side.[17][11]
Design and manufacture[]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/f/f8/Engineers_and_Technicians_Load_Test_Coupons_into_the_Environmental_Test_Facility.jpg/220px-Engineers_and_Technicians_Load_Test_Coupons_into_the_Environmental_Test_Facility.jpg)
Northrop Grumman designed the sunshield for NASA.[18] The sunshield is designed to be folded twelve times so it can fit within the Ariane 5 rocket's 4.57 m (15.0 ft) diameter by 16.19 m (53.1 ft) shroud. When it deployed at the L2 point, it unfolded to 21.197 m × 14.162 m (69.54 ft × 46.46 ft). The sunshield was hand-assembled at ManTech (NeXolve) in Huntsville, Alabama before it was delivered to Northrop Grumman in Redondo Beach, California for testing.[19] During launch it was wrapped around the Optical Telescope Element and then later unfolded.[11] The sunshield was planned to be unfolded approximately one week after launch.[20] During development the sunshield layer material was tested with heat, cold, radiation, and high-velocity micro impacts.[10]
Components of the sunshield include:[21]
- Core
- Front and aft four-bar linkage
- Aft structure assembly
- Momentum trim tab (the tab is attached to the aft structure assembly)
- Aft spreader bars (spreads layers in the rear)
- Forward structure assembly
- Forward spreader bars
- Mid-booms (one on each side)
- Mid-spreader bars (spreads the 5 layers apart)
- Two forward and two aft bipod launch lock assemblies
The bipod launch lock assemblies are where the sunshield segment connected to the OTE when it was folded up during launch.[21] There are six spreader bars that expanded to separate the layers of the sunshield, which has roughly six sides.[21]
Trim flap/momentum trim tab[]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/a/a8/JWST-pointing-and-roll-limits.png/220px-JWST-pointing-and-roll-limits.png)
The sunshield segment also includes a trim flap at the end of a sunshield deployment boom.[3] This is also called the momentum trim tab.[21] The trim tab helps balance out solar pressure caused by photons striking the sunshield. If this pressure is uneven, the spacecraft will tend to rotate, requiring its reactions wheels to correct and actively maintain its orientation in space, which consumes power. The trim tab helps to keep the pressure balanced across the entire telescope passively without fuel or power, extending the working life of the telescope.[how?][22][21][3][23] The trim tab also manages the effects of the reaction wheels.[how?][3] The reaction wheels are located in the spacecraft bus.
Layers[]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/d/dc/James_Webb_Space_Telescope_Sunshield_Test_Unfolds_Seamlessly_%2815235550340%29.jpg/220px-James_Webb_Space_Telescope_Sunshield_Test_Unfolds_Seamlessly_%2815235550340%29.jpg)
The layer nearest to primary mirror, layer 5, is the only one with a line of sight to the mirror, while the layer closest to the Sun, layer 1, is the only one that receives direct sunlight.[4] The separation between layers, in the vacuum of space, prevents heat transfer by conduction and aids in radiating heat out of the way.[24]
The silicon doping is what causes the purple hue of the areas covered with that material.[24]
The layers are designed so the Sun, Earth, and Moon shine on layer 1 almost exclusively, sometimes a tiny portion of layer 2, and on the other side that the telescope elements only see layer 5 and sometimes a tiny amount of layer 4.[21]
Dimensions of the individual layers are:[4]
- Largest area[4]
- 0.050 mm (0.002 in)
- 100 nm (3.9 μin) aluminum coating (both sides)
- 50 nm (2.0 μin) doped silicon
-
- 0.025 mm (0.001 in)
- 100 nm (3.9 μin) aluminum coating (both sides)
- 50 nm (2.0 μin) doped silicon
-
- 0.025 mm (0.001 in)
- 100 nm (3.9 μin) aluminum coating (both sides)
-
- 0.025 mm (0.001 in)
- 100 nm (3.9 μin) aluminum coating (both sides)
- Smallest area[4]
- 0.025 mm (0.001 in)
- 100 nm (3.9 μin) aluminum coating (both sides)
Deployment[]
The sunshield component attaches to the main spacecraft, and its booms expand outward spreading out the heat shield and separating the layers.[25] During launch the shield is folded up; later, when it is in space, it is carefully unfurled.[25] When the sunshield is fully spread open, it is 14.6 meters (48 ft) wide by 21.1 meters (69 ft) long.[21] When the layers are fully open, they are opened wider at the edges which helps reflect heat out.[21]
Sunshield deployment structure/devices include:[24]
- telescoping booms
- stem deployers
- spreader bars
- cable drives
There are two stem deployers inside the telescoping booms.[24] These are special electrical motors that, when operated, extended the telescopic boom, pulling out the folded sunshield.[24] The telescopic booms are called the MBA, or mid-boom assemblies.[21] At the end of each MBA is a spreader bar.
After a successful launch on 2021 December 25 from the Guiana Space Center, the post-launch deployment of the JWST sunshield proceeded as follows.
On 2021 December 31, the ground team at the Space Telescope Science Institute in Baltimore, Maryland began the deployment of the two telescoping "mid booms" from the left and right sides of the observatory, pulling the five sunshield membranes out of their folded stowage in the fore and aft pallets, which were lowered three days earlier.[26] Deployment of the left side boom (in relation to pointing direction of the main mirror) was delayed when mission control did not initially receive confirmation that the sunshield cover had fully rolled up. After looking at extra data for confirmation, the team proceeded to extend the booms.[27] The left side deployed in 3 hours and 19 minutes; the right side took 3 hours and 42 minutes.[27][26] With that step, Webb's sunshield resembled its complete, kite-shaped form and extended to its full 47-foot width. Commands to separate and tension the membranes were to follow.[26]
After taking New Year's Day off, the ground team delayed sunshield tensioning by one day to allow time to optimize the power output of the observatory's array of solar panels and to adjust the orientation of the observatory to cool the slightly-hotter-than-expected sunshield deployment motors.[28] Tensioning of layer one, closest to the Sun and largest of the five in the sunshield, began on 2022 January 3 and was completed at 3:48 p.m. EST.[29] Tensioning of the second and third layers began at 4:09 p.m. EST and took 2 hours and 25 minutes.[30] On 2022 January 4, controllers successfully tensioned the last two layers, four and five, completing the task of deploying the JWST sunshield at 11:59 a.m. EST.[31]
Timeline[]
- 2007 or before, Technology Readiness Level (TRL) 6 achieved for the sunshield membrane.[14]
- 2016 September 11, first layer of sunshield completed.[12]
- 2016 November 2, the final fifth layer is completed.[32]
- 2018 March 27, NASA announced the presence of tears in the sunshield, contributing to launch delays.[33]
- 2021 December 25, successful launching of the James Webb Space Telescope from the Guiana Space Center.[34]
- 2021 December 31, initial deployment of the telescoping booms to support and unfurl the sunshield.[35]
- 2022 January 3, initial tensioning and separating of the first three layers of the sunshield.[36]
- 2022 January 4, completion of tensioning/separating all five layers and the successful deployment of the JWST sunshield, ten days after launch and more than 0.8 million kilometers (500,000 mi) away from Earth.[1][36][35]
See also[]
- James Webb Space Telescope timeline
- Skylab (also used deployed expanding fabric/layer sun-shield in the 1970s)
- Spacecraft thermal control
- New Worlds Mission (also blocks sunlight, but for observing exoplanets obscured by their bright parent star)
- Insulation
- Heat shield
References[]
- ^ a b "Sunshield Successfully Deploys on NASA's Next Flagship Telescope". nasa.gov. Retrieved January 4, 2022.
- ^ Dunn, Marcia (January 5, 2022). "NASA nails trickiest job on newly launched space telescope". thestar.com. Toronto Star. Retrieved January 5, 2022.
- ^ a b c d "The Webb Update #5". The James Webb Space Telescope. National Aeronautics and Space Administration. September 2008. Archived from the original on October 13, 2008.
{{cite web}}
: CS1 maint: unfit URL (link) - ^ a b c d e f g h i j k l m n o p "About The Sunshield". jwst.nasa.gov. Retrieved December 27, 2021.
- ^ a b c d e f "Sunshield Membrane Coatings". James Webb Space Telescope. NASA. Retrieved December 27, 2021.
- ^ "The Sunshield Webb/NASA". webb.nasa.gov. Retrieved December 30, 2021.
- ^ "A Solar Orbit". jwst.nasa.gov. Retrieved August 28, 2016.
- ^ "L2 Orbit". Space Telescope Science Institute. Archived from the original on February 3, 2014. Retrieved August 28, 2016.
- ^ Schupak, Amanda (December 17, 2021). "NASA's James Webb Space Telescope Will Take Us Back to the Dawn of the Cosmos". The Daily Beast.
- ^ a b Gutro, Rob (November 12, 2008). "Super-Tough Sunshield to Fly on the James Webb Space Telescope". NASA. Retrieved December 27, 2021.
- ^ a b c d "Sunshield". Space Telescope Science Institute.
{{cite web}}
: CS1 maint: url-status (link)[dead link] - ^ a b "JWST sunshield". Huntsville, Ala.: Nexolve. Archived from the original on December 21, 2016. Retrieved December 6, 2016.
- ^ a b c Ferreira, Becky (October 20, 2014). "This Sunshield Will Keep the World's Most Powerful Space Telescope from Frying". Vice.
- ^ a b c Lo, Amy. The James Webb Space Telescope (PDF) (Report). 2015 US Frontiers of Engineering: Engineering the Search for Earth-like Exoplanets. Retrieved December 27, 2021.
- ^ Willey, Scott (December 10, 2015). "Restoring the Apollo Telescope Mount". National Air and Space Museum. Retrieved July 12, 2018.
When we uncrated the spar in September 2014, we discovered that after 40 years the Kapton®—the shiny, crinkly material you can often see on satellites and in this case the black material you can see in our photos—was in really poor condition.
- ^ Clery, Daniel (March 27, 2018). "NASA announces more delays for giant space telescope". Science. Retrieved June 5, 2018.
- ^ Potter, Sean (January 4, 2022). "Sunshield Successfully Deploys on NASA's Next Flagship Telescope". NASA. Retrieved February 11, 2022.
- ^ "NASA James Webb Space Telescope's Sunshield Successfully Unfolds and Tensions in Final Tests". SciTechDaily. December 20, 2020. Retrieved December 27, 2021.
- ^ Morring, Frank Jr. (December 16, 2013). "JWST Sunshade Folding, Deployment In Test". Aviation Week & Space Technology. pp. 48–49. ISSN 0005-2175.
- ^ "About Webb Orbit". NASA. Retrieved January 2, 2022.
- ^ a b c d e f g h i Arenberg, J.; Flynn, J.; Cohen, A.; Lynch, R.; Cooper, J. (August 9, 2016). MacEwen, Howard A; Fazio, Giovanni G; Lystrup, Makenzie; Batalha, Natalie; Siegler, Nicholas; Tong, Edward C (eds.). "Status of the JWST sunshield and spacecraft" (PDF). Society of Photo-Optical Instrumentation Engineers (SPIE). Space Telescopes and Instrumentation 2016: Optical, Infrared, and Millimeter Wave. 9904: 990405. Bibcode:2016SPIE.9904E..05A. doi:10.1117/12.2234481. S2CID 126299529. Archived from the original (PDF) on December 21, 2016. Retrieved March 28, 2018.
- ^ "James Webb Space Telescope's Aft Momentum Flap Deployed". SciTechDaily. Retrieved January 6, 2022.
- ^ Kinzel, Wayne. "Momentum Management Operations Concept". CiteSeerX. Space Telescope Science Institute. Retrieved February 15, 2008.
- ^ a b c d e "Testing the Fold: The James Webb Space Telescope's Sunshield". NASA. December 3, 2012. Retrieved January 20, 2017.
- ^ a b "Super-Tough Sunshield to Fly on the James Webb Space Telescope". NASA. Retrieved January 20, 2017.
- ^ a b c Lynch, Patrick (December 31, 2021). "With Webb's Mid-Booms Extended, Sunshield Takes Shape". James Webb Space Telescope (NASA Blogs). Retrieved January 1, 2022.
- ^ a b Lynch, Patrick (December 31, 2021). "First of Two Sunshield Mid-Booms Deploys". James Webb Space Telescope (NASA Blogs). Retrieved January 1, 2022.
- ^ Zastrow, Mark (January 5, 2022). "James Webb Space Telescope successfully deploys sunshield". astronomy.com. Retrieved January 5, 2022.
- ^ Fox, Karen (January 3, 2022). "First Layer of Webb's Sunshield Tightened". James Webb Space Telescope (NASA Blogs). Retrieved January 4, 2022.
- ^ Lynch, Patrick (January 3, 2022). "Second and Third Layers of Sunshield Fully Tightened". James Webb Space Telescope (NASA Blogs). Retrieved January 4, 2022.
- ^ Fox, Karen (January 4, 2022). "Webb Team Tensions Fifth Layer, Sunshield Fully Deployed". James Webb Space Telescope (NASA Blogs). Retrieved January 5, 2022.
- ^ Sharkey, Jim (November 2, 2016). "Final layer of sunshield completed for NASA's James Webb Space Telescope". SpaceFlight Insider.
- ^ Lewin, Sarah (March 27, 2018). "NASA Delays Launch of James Webb Space Telescope Until 2020". Space.com. Retrieved March 28, 2018.
- ^ "NASA's Webb Telescope Launches to See First Galaxies, Distant Worlds". nasa.gov. Retrieved January 4, 2022.
- ^ a b Dickinson, David (January 4, 2022). "CRITICAL STEP COMPLETE AS WEBB SPACE TELESCOPE DEPLOYS SUNSHIELD". skyandtelescope.org. Retrieved January 4, 2022.
- ^ a b Clark, Stephen (January 5, 2022). "'We nailed it!' Webb clears major hurdle with full sunshade deployment". astronomynow.com. Retrieved January 5, 2022.
External links[]
![]() |
Wikimedia Commons has media related to Sunshield (JWST). |
- James Webb Space Telescope