Optical Telescope Element (OTE) is one of three major sections of the James Webb Space Telescope, a large infrared space telescope launched on 25 December 2021, consisting of its main mirror, secondary mirrors, the framework and controls to support the mirrors, and various thermal and other systems. The OTE collects the infrared light and directs it to the science instruments in Webb's second major section, the Integrated Science Instrument Module (ISIM). The OTE has been compared to being the "eye" of the telescope and the backplane of it to being the "spine". The third major section of the JWST is the Spacecraft Element (SE), which includes the spacecraft bus and sunshield. The OTE has a three-mirror anastigmat (TMA) design, with an effective f/20 focal ratio and focal length of 131.4 meters (431 ft). The primary mirror is a tiled assembly of 18 hexagonal elements, each 1.32 meters (4.3 ft) from flat to flat. When properly aligned, this combination yields an effective aperture of 6.5 meters (21 ft) and a total collecting surface of 25.4 square meters (273 ft2). The secondary mirror is a convex circular mirror with a diameter of 0.74 meters (2.4 ft), and it feeds into the Aft Optics Subsystem (part of OTE), which contains the tertiary mirror (fixed) and the Fine Steering Mirror (FSM, movable). All mirrors are made of gold-plated beryllium, due to its low weight, structural stability at low temperatures and high infrared reflectivity. The principal subcontractor for the JWST optics was Ball Aerospace, and the mirror development team included Brush Wellman (forming), Axsys Technologies (shaping) and L-3 Communications SSG-Tinsley (polishing). The components of OTE were integrated by L3Harris Technologies to form the final system.
Overview
The OTE combines a large amount of the optics and structural components of the James Webb Space Telescope, including the Main mirror. It also has the fine steering mirror, which provides that final precise pointing, and it works in conjunction with the fine guidance sensor and other controls systems and sensors in the spacecraft bus. The main mirror segments are aligned roughly using a coarse phasing algorithm. Then for finer alignment, special optical devices inside NIRCam are used to conduct a phase retrieval technique, to achieve designed wavefront error of less than 150 nm. To function as focusing mirror correctly the 18 main mirror segments need to be aligned very closely to perform as one. This needs to be done in outer space, so extensive testing on Earth is required to ensure that it will work properly. To align each mirror segment, it is mounted to six actuators that can adjust that segment in 5 nm steps. One reason the mirror was divided into segments is that it cuts down on weight, because a mirror's weight is related to its size, which is also one of the reasons beryllium was chosen as the mirror material because of its low weight. Although in the essentially weightless environment of space the mirror will weigh hardly anything, it needs to be very stiff to maintain its shape. The Wavefront sensing and control sub-system is designed to make the 18 segment primary mirror behave as a monolithic (single-piece) mirror, and it does this in part by actively sensing and correcting for errors. There are nine distance alignment processes that the telescope goes through to achieve this. Another important aspect to the adjustments is that the primary mirror backplane assembly is steady. The backplane assembly is made of graphite composite, invar, and titanium. The ADIR, Aft Deployable Infrared Radiator is a radiator behind the main mirror, that helps keep the telescope cool. There are two ADIR's and they are made of high-purity aluminum. There is a special black coating on the radiators that helps them emit heat into space.
Some major parts of the OTE according to NASA:
Primary mirror (18 segments) Secondary mirror (74 cm (29 in) diameter) Tertiary mirror (3rd) (in Aft Optics Subsystem) Fine Steering Mirror (in Aft Optics Subsystem) Telescope structure primary mirror backplane assembly main backplane support fixture (BSF) secondary mirror support structure deployable tower array Thermal Management Subsystem Aft Deployable ISIM Radiator (ADIR) Wavefront sensing and control The Aft Optics Subsystem includes the Tertiary mirror and the Fine Steering Mirror. One of the tasks for the Fine steering mirror is image stabilization. The metal beryllium was chosen for a number of reasons including weight, but also for its low-temperature coefficient of thermal expansion compared to glass. Furthermore beryllium is not magnetic and a good conductor of electricity and heat. Other infrared telescopes that have used beryllium mirrors include IRAS, COBE, and Spitzer. The Subscale Beryllium Model Demonstrator (SBMD) was successfully tested at cryogenic temperatures, and one of the concerns was surface roughness at low kelvin numbers. The beryllium mirrors are coated with a very fine layer of gold to reflect infrared light. There are 18 hexagonal segments that are grouped together to create a single mirror with an overall diameter of 6.5 meters (21 ft).
DTA
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