Structural Analysis Technique and Its Validation for Large Range Mirror Refocusing System for Spaceborne Deployable Telescopes

Authors

  • Yesh Pal Space Applications Centre, Indian Space Research Organization, India
  • Rahul Dev Space Applications Centre, Indian Space Research Organization, India
  • Naimesh R. Patel Space Applications Centre, Indian Space Research Organization, India
  • Neeraj Mathur Space Applications Centre, Indian Space Research Organization, India
  • Shaunak R. Joshi Space Applications Centre, Indian Space Research Organization, India
  • Harshraj Dod Lalbhai Dalpatbhai College of Engineering, India

DOI:

https://doi.org/10.47852/bonviewJOPR42022660

Keywords:

mirror, telescope, displacement, refocusing, stiffness, direction

Abstract

Large aperture deployable telescopes with numerous onboard instruments are popular in the space industry for astronomy. Scientific data in various wavelength bands, from 0.6µ to 28µ, is provided by these instruments and is crucial for deep space exploration. The deployment mechanisms handle the alignment and functionality at the telescope level only. At instrument level, there is always a need for a refocusing system which can cater individual need of instrument for focusing independent to other instruments nearby. In this paper, we present a structural analysis technique for such a type of large range mirror refocusing mechanism, similar to the Near Infrared Spectrograph (NIRSpec) payload of the James Webb Space Telescope (JWST). The method relies on geometric non-linearity for large deflection, in which the structure's stiffness matrix changes as a function of loading. We have designed, analyzed structurally, and tested a 4mm range slider crank based compliant mechanism. The outcomes of linear and non-linear static analysis, computed numerically, have been compared. There are noticeable significant variations in one direction between the two analyses' results. The results are validated using appropriately designed and realized test setups, like measurements of displacement, changes in focus and image position of the optical system.

 

Received:  21 February 2024 | Revised: 15 May 2024 | Accepted: 1 October 2024

 

Conflicts of Interest

The authors declare that they have no conflicts of interest to this work.

 

Data Availability Statement

The data that support the findings of this article cannot be publicly available due to privacy. They can be requested from the corresponding author.

 

Author Contribution Statement

Yesh Pal: Conceptualization, Methodology, Software, Validation, Formal analysis, Investigation, Resources, Data curation, Writing - original draft, Writing - review & editing, Visualization, Project administration. Rahul Dev: Conceptualization, Methodology, Validation, Investigation, Resources, Data curation, Writing - review & editing, Visualization, Supervision, Project administration. Naimesh R. Patel: Conceptualization, Methodology, Software, Validation, Formal analysis, Investigation, Resources, Data curation, Writing - review & editing, Visualization, Supervision, Project administration. Neeraj Mathur: Conceptualization, Investigation, Resources, Writing - review & editing, Supervision, Project administration. Shaunak R. Joshi: Conceptualization, Investigation, Resource, Writing - review & editing, Supervision, Project administration. Harshraj Dod: Software, Validation, Formal analysis, Investigation, Writing - original draft, Writing - review & editing.


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Published

2024-10-08

Issue

Section

Research Articles

How to Cite

Pal, Y. ., Dev, R. ., Patel, N. R. ., Mathur, N. ., Joshi, S. R. ., & Dod, H. . (2024). Structural Analysis Technique and Its Validation for Large Range Mirror Refocusing System for Spaceborne Deployable Telescopes. Journal of Optics and Photonics Research. https://doi.org/10.47852/bonviewJOPR42022660