Integrated Science Instrument Module Research Articles

The Design, Verification, and Performance of the James Webb Space Telescope

The James Webb Space Telescope (JWST) is NASA’s flagship mission successor to the highly successful Hubble Space Telescope. It is an infrared observatory featuring a cryogenic 6.6 m aperture, deployable Optical Telescope Element (OTE) with a payload of four science instruments (SIs) assembled into an Integrated Science Instrument Module (ISIM) that provide imagery and spectroscopy in the near-infrared band between 0.6 and 5 μm and in the mid-infrared band between 5 and 28.1 μm. JWST was successfully launched on 2021 December 25 aboard an Ariane 5 launch vehicle. All 50 major deployments were successfully completed on 2022 January 8. The observatory performed all midcourse correction maneuvers and achieved its operational mission orbit around the Sun–Earth second Lagrange point (L2). All commissioning and calibration activities have been completed, and JWST has begun its science mission. This paper will provide a description of the driving requirements and their technical challenges, the engineering processes involved in the design formulation, the resulting observatory design, the verification programs that proved it to be flightworthy, and the measured on-orbit performance of the observatory. Since companion papers will describe the details of the OTE and SIs, this paper will concentrate on describing the key features of the observatory architecture that accommodates these elements, particularly those features and capabilities associated with accommodating the radiometric and image-quality performance.

Use of close range photogrammetry in James Webb Space Telescope alignment testing under cryogenic conditions

The James Webb Space Telescope (JWST) cryogenic testing required measurement systems that both obtain a very high degree of accuracy and can function in that environment. Close-range photogrammetry was identified as meeting those criteria. Extensive modeling prior to installation verified that the design would meet the desired accuracy goals. Extensive validation work was done to ensure that the actual as-built system met accuracy and repeatability requirements. The simulated image data predicted the uncertainty in measurement to be within specification and this prediction was borne out experimentally. Uncertainty at all levels of a measurement volume that comprised 8 × 8 m was verified experimentally to be <0.1 mm with a repeatability of <0.03 mm at the primary mirror (PM) level, achieving measurement accuracies on par with a laser tracker or radar system. During a 3-month Optical Telescope Element and Integrated Science Instrument Module thermal vacuum test performed in chamber A at Johnson Space Center, the photogrammetric system provided key data to allow for verification of actuator ranges needed for on-orbit alignment of JWST, alignment of the PM and secondary mirror (SM), and positional information needed for thermal model verification.