To make observations in the near and mid infrared spectrum, the JWST must be kept very cold (under , some parts under 40K), 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 Lagrange point keeps all three bodies on the same side of the spacecraft at all times. Its
halo orbit around L2 avoids the shadow of the Earth and Moon, maintaining a constant environment for the sunshield and solar arrays. The sunshield acts as large
parasol allowing the main mirror, optics, and instruments to
passively cool to or cooler, and is one of the enabling technologies that will allow the JWST to operate. The kite-shaped sunshield is about in size, from front to back. The sunshield has five layers to mitigate the conduction of heat. and Kapton is known to degrade after long term exposure to Earth conditions. The sun-facing layer is thick, and the other layers are thick. All layers are coated on both sides with 100 nm of
aluminum, and the Sun-facing sides of the outermost two layers are also coated with 50 nm of
silicon "
doped" with other elements. 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. The sunshield allows the optics to stay in shadow for pitch angles of +5° to −45° and roll angles of +5° to −5°. The layers are designed with Thermal Spot Bond (TSB), with a grid pattern bonded to each layer at intervals. This helps stop a rip or hole from increasing in size should one occur. ==Design and manufacture==