Designing a Telescope for Laser Communication with Ceramic Matrix Composites

Evaluating the viability of C/C-SiC for thermally stable space optics

Master Thesis (2025)
Author(s)

G.H.M. Hartman (TU Delft - Aerospace Engineering)

Contributor(s)

D.M.J. Peeters – Mentor (TU Delft - Group Peeters)

Jan de Vreugd – Mentor (TNO)

Y. Tang – Graduation committee member (TU Delft - Group Tang)

R. Saathof – Graduation committee member (TU Delft - Space Systems Egineering)

Faculty
Aerospace Engineering
More Info
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Publication Year
2025
Language
English
Graduation Date
29-09-2025
Awarding Institution
Delft University of Technology
Programme
['Aerospace Engineering']
Sponsors
TNO
Faculty
Aerospace Engineering
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Abstract

Carbon–carbon silicon carbide (C/C–SiC) is a ceramic matrix composite combining low density with high stiffness, damage tolerance, and excellent thermal properties. A feature of this material is its low (0.1𝜇m/mK) and tunable coefficient of thermal expansion (CTE), making it highly suitable for precision structures that must remain dimensionally stable under varying thermal loads. This thesis investigates its applicability to a 100 mm diameter Cassegrain telescope structure as a candidate for space-based laser communication terminals. A parametric thermo-elastic finite element model was developed in COMSOL Multiphysics. Rigid body motions and surface form errors were quantified using a Zernike-polynomial-based Python post-processing pipeline, enabling evaluation of optical performance. Results show that by targeting a near-zero in-plane CTE, C/C–SiC can maintain deformations within acceptable limits, supporting its feasibility for lightweight and stable free-space optical communication
systems. Using an opto-thermo-mechanical workflow, the model couples radiative and conductive heat transfer with the structural response to assess wavefront stability under representative orbital thermal load cases. Within the evaluated steady-state cases, tuning the in-plane CTE to approximately 0.1–0.5 𝜇m/mK kept rigid-body motions and surface-form errors within a 𝜆/30 ≈ 50 nm RMS budget, leaving margin for other effects treated as out of scope. From a production perspective, however, current cleanliness and manufacturing-consistency challenges for large continuous-fiber C/C–SiC constrain near-term applicability to off-the-shelf terminals, suggesting more viable deployment in other use cases until maturity improves.

http://10.4121/e139a134-6bd2-4298-932d-975356efd964
Location of the models and post-processing scripts

Files

GHMH_Thesis_report.pdf
(pdf | 86.7 Mb)
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