TY - JOUR
T1 - Multi-facial freeform monolith optics for astronomical and space applications
AU - Kumar, Sumit
AU - Zhong, Wenbin
AU - Kumar, Prashant
AU - Scott, Paul
AU - Jiang, Jane
AU - Zeng, Wenhan
N1 - Funding Information:
The authors gratefully acknowledge the United Kingdom\u2019s Engineering and Physical Sciences Research Council (EPSRC) funding of Future Metrology Hub (Ref: EP/P006930/1), the United Kingdom\u2019s Science and Technology Facilities Council (STFC) Innovation Partnership Scheme (IPS) projects under grant agreement No. ST/V001280/1, and ST/W005263/1.
Funding Information:
The authors gratefully acknowledge the United Kingdom's Engineering and Physical Sciences Research Council (EPSRC) funding of Future Metrology Hub (Ref: EP/P006930/1), the United Kingdom's Science and Technology Facilities Council (STFC) Innovation Partnership Scheme (IPS) projects under grant agreement No. ST/V001280/1, and ST/W005263/1.The authors declare the following financial interests/personal relationships which may be considered as potential competing interests: Xiangqian Jiang, Paul Scott, Wenhan Zeng, Wenbin Zhong, Prashant Kumar, Sumit Kumar reports financial support was provided by Engineering and Physical Sciences Research Council. Wenbin Zhong, Wenhan Zeng reports financial support was provided by Science and Technology Facilities Council. If there are other authors, they declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.The authors would like to acknowledge the scholarship received from the United Kingdom's EPSRC Future Metrology Hub (Ref.: EP/P006930/1) on Mr. Sumit Kumar's PhD research.
Funding Information:
The authors would like to acknowledge the scholarship received from the United Kingdom\u2019s EPSRC Future Metrology Hub (Ref.: EP/P006930/1) on Mr. Sumit Kumar\u2019s PhD research.
Publisher Copyright:
© 2024 The Authors
PY - 2024/11/26
Y1 - 2024/11/26
N2 - The utilization of a multi-facial freeform monolithic (MFFM) component in a compact Cassegrain configuration design offers unprecedented capabilities to accommodate various next-generation science instruments. The concept of the MFFM component can be employed for applications in telescopes working at ultra-violet, optical, infrared, terahertz, microwave, and even radio frequencies. MFFM finds its scope in space optical and astronomical systems where the risks are associated with the alignment, manufacturability, and maintaining large-sized apertures, large number of components, cost, and volume of the flight optical terminals and instruments. The current challenges faced at the manufacturing phase of MFFM are the precision positioning of each surface concerning the optical axis and maintaining the required edge thickness. This paper presents the optical design, fabrication, measurement, and in-laboratory characterization of MFFM. The results of a prototyping effort through ultra-precision single-point diamond turning (SPDT) and coating demonstrate the feasibility of producing these elements as per size and weight requirements. The experimental results show excellent surface qualities in terms of nanometric surface roughness and close-to-submicron form accuracy on each surface of the freeform monolith. Focusing performance and imaging performance are carried out to validate the designed and manufactured precision component. The main contribution is highlighted in terms of the optimized fabrication process for producing the precision MFFM for a fast optical system while balancing the alignment errors. The demonstrated research work highlights the intriguing possibilities of the monolith and creates new avenues for research in domains that use huge optical systems, such as astrophysical study, planetary observation, earth monitoring, and geosciences.
AB - The utilization of a multi-facial freeform monolithic (MFFM) component in a compact Cassegrain configuration design offers unprecedented capabilities to accommodate various next-generation science instruments. The concept of the MFFM component can be employed for applications in telescopes working at ultra-violet, optical, infrared, terahertz, microwave, and even radio frequencies. MFFM finds its scope in space optical and astronomical systems where the risks are associated with the alignment, manufacturability, and maintaining large-sized apertures, large number of components, cost, and volume of the flight optical terminals and instruments. The current challenges faced at the manufacturing phase of MFFM are the precision positioning of each surface concerning the optical axis and maintaining the required edge thickness. This paper presents the optical design, fabrication, measurement, and in-laboratory characterization of MFFM. The results of a prototyping effort through ultra-precision single-point diamond turning (SPDT) and coating demonstrate the feasibility of producing these elements as per size and weight requirements. The experimental results show excellent surface qualities in terms of nanometric surface roughness and close-to-submicron form accuracy on each surface of the freeform monolith. Focusing performance and imaging performance are carried out to validate the designed and manufactured precision component. The main contribution is highlighted in terms of the optimized fabrication process for producing the precision MFFM for a fast optical system while balancing the alignment errors. The demonstrated research work highlights the intriguing possibilities of the monolith and creates new avenues for research in domains that use huge optical systems, such as astrophysical study, planetary observation, earth monitoring, and geosciences.
KW - Freeform optics
KW - Multi-facial monolith
KW - Ultra-precision manufacturing
KW - Astronomical and space
KW - Imaging optics
UR - http://www.scopus.com/inward/record.url?scp=85209987397&partnerID=8YFLogxK
U2 - 10.1016/j.optcom.2024.131345
DO - 10.1016/j.optcom.2024.131345
M3 - Article
VL - 576
JO - Optics Communications
JF - Optics Communications
SN - 0030-4018
M1 - 131345
ER -