Abstract

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.

Highlights

  • Close range photogrammetry has successfully been used on large hardware systems such as the microwave anisotropy probe[1] for dimensional surveys of large numbers of points

  • Given the demonstrated ability of photogrammetry (PG) to operate in such an environment to similar tolerances, it was chosen for use as the Cryo-Position Metrology (CPM) system for the Optical Telescope Element and Integrated Science Instrument Module (ISIM) (OTIS) thermal vacuum (T/V) tests to be performed in chamber A at Johnson Space Center (JSC)

  • The origin is the center of the base of the Aft Optics Subsystem (AOS) on the primary mirror (PM) and the axis is oriented as shown in Fig. 1 where +M1 is toward the top of the chamber, and +M2/ +M3 are in the plane of the PM

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Summary

Introduction

Close range photogrammetry has successfully been used on large hardware systems such as the microwave anisotropy probe[1] for dimensional surveys of large numbers of points. Given the demonstrated ability of photogrammetry (PG) to operate in such an environment to similar tolerances, it was chosen for use as the Cryo-Position Metrology (CPM) system for the Optical Telescope Element and ISIM (OTIS) thermal vacuum (T/V) tests to be performed in chamber A at Johnson Space Center (JSC). Predictions were compared to subsequent verification measurements of the operational CPM performed during initial chamber tests of ground support equipment (GSE) to be used in the full OTIS tests. These tests are designated as chamber commissioning test (CCT), OGSE1 and OGSE2 (optical GSE), and thermal pathfinder (TPF) in this paper. This would not have been possible without the pretest computer models and extensive JWST pathfinder testing at under cryogenic conditions

Value of the PG System for JWST
CPM Hardware Description
Scale Bars
Coded Targets
INCA Camera System
Coordinate System
Data Processing
Modeled Imagery Generation
Modeled Image Results and Applications
Prediction of PG Accuracy
Repeatability
SM measurement cross checks
Alignment of PM and SM
Conclusions
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