NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Influence of Core and Hexapod Geometry, and Local Reinforcement on the Performance of Ultra-Lightweight ULE MirrorThe Habitable Exoplanet Observatory (HabEx) mission has unique optical performance requirements which drive the mirror design process beyond the traditional criteria. While mass and stiffness are still important, the response to inertia loading (expressed in terms of Zernike coefficients) to omni-directional excitation dominates the effort. While a Zerodur mirror is the current baseline, as mass budgets change, a ULE design is being studied as a potential alternative. This trade study looked at over 264 design variations using the Arnold Mirror Modeler and ANSYS(c) to investigate the influence of various design elements, including: substrate thickness, core cell size, hexapod geometry and local reinforcement. Design 'goodness' was evaluated based on the mirror's inertial deformation response to omni-directional input. This response was calculated via RSSing Zernike polynomial responses to (XYZ) accelerations.
Document ID
20180006819
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
External Source(s)
Authors
Arnold, William R.
(AI Solutions, Inc. Lanham, MD, United States)
Stahl, H. Phillip
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
October 24, 2018
Publication Date
August 19, 2018
Subject Category
Space Sciences (General)
Report/Patent Number
MSFC-E-DAA-TN61193
Report Number: MSFC-E-DAA-TN61193
Meeting Information
Meeting: Optics and Photonics Conference Proceedings
Location: San Diego, CA
Country: United States
Start Date: August 19, 2018
End Date: August 23, 2018
Sponsors: International Society for Optical Engineering
Funding Number(s)
CONTRACT_GRANT: NNM14AA89D
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Space Telescope Technology
No Preview Available