DICOS is a technological demonstrator under a stratospheric balloon for advanced pointing and wavefront stability technologies. The aim is to reach 10 mas fine pointing and 20 nm rms wavefront error (WFE), with 1 nm rms stability. The sizing case comes from the coronography technique for exoplanets direct detection. The instrument is based on a 40 cm telescope made in aluminum and mounted in a CARMEN gondola. The deformations and pointing errors are compensated by active loops driving a deformable mirror (DM) with 97 actuators. The current funded phase of the project will end in 2024 by a full-scale ground demonstration.
Silicon nitride is a ceramic material that has very interesting stability properties for space telescopes. Indeed, the objective for telescopes is chiefly stability and with its high strength and stiffness and low CTE, Silicon Nitride is well suited for complex space structures. Thales Alenia Space has demonstrated the ability of Si3N4 to address those needs and requirements for complex designs such as tubes, brackets, brazed supports and bars. All these structures have been tested, qualified and flight proven. In addition, deep characterization of the material strength has been performed. Now that this material has been demonstrated as suitable for telescope structures, several R&D activities are pursued, from production via additive manufacturing to suitability for optical parts. This paper shows an overview of past, on-going and foreseen developments for the Silicon Nitride technology.
Zerodur® is a well-known glass-ceramic used for optical components because of its unequalled dimensional stability
under thermal environment. In particular it has been used since decades in Thales Alenia Space’s optical payloads for
space telescopes, especially for mirrors. The drawback of Zerodur® is however its quite low strength, but the relatively
small size of mirrors in the past had made it unnecessary to further investigate this aspect, although elementary tests have
always shown higher failure strength. As performance of space telescopes is increasing, the size of mirrors increases
accordingly, and an optimization of the design is necessary, mainly for mass saving. Therefore the question of the
effective strength of Zerodur® has become a real issue.
Thales Alenia Space has investigated the application of the Weibull law and associated size effects on Zerodur® in 2014,
under CNES funding, through a thorough test campaign with a high number of samples (300) of various types. That test
campaign demonstrated a strength in fast fracture higher than 40 MPa ([1], [2]) for the tested surface finish, thus
allowing much more versatility in the designs than the previously accepted strength limit (10 MPa).
Another concern had however been raised: glasses are known to be susceptible to sub-critical crack growth, i.e. slow
propagation of cracks under loads below fracture toughness, thus reducing fast fracture strength capabilities (since failure
is linked to sudden propagation of those cracks). Taking into account data from literature, no effect was expected on
Zerodur® in the conditions of use for space applications, but the very high variability of data made those computations
not reliable enough. A dedicated test campaign was therefore defined in order to assess this effect and its consequences
in conditions as representative as possible of real conditions.
In this paper we show the outcome of this test campaign: the effect of subcritical crack growth is confirmed to be
negligible and the minimum strength of 40 MPa is confirmed. In time, Zerodur® strength seems to even increase but this
phenomenon was not investigated in the study.
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