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Cryogenic Deformable Mirror Technology Development

机译:低温变形镜技术发展

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Xinetics is working with NASA to develop a cryogenic deformable mirror (DM) specific to the needs of future Origins Program missions such as TPF and JWST. Of utmost importance was the development of an electroceramic material that exhibited electrostrictive properties at cryogenic temperatures. In this paper, the actuator developmental tests and subsequent cryogenic deformable mirror design and cryogenic testing performance of the 349-channel discrete actuator deformable mirror demonstrator are discussed. The cofired actuator stroke response was nearly constant from 35 to 65 K such that at 150V the actuator free-stroke was ~3 microns. The 349-ch cryogenic DM was designed and built with as few parts and materials as possible to minimize the CTE mismatch. The polished mirror was cycled twice from 300 to 35 K. The rms surface figure was monitored using a Zygo interferometer on cooling and consistent data was measured during both temperature cycles. The figure changed from 0.5 waves (P-V) at 300 K to 5 waves at 35 K and returned to 0.6 waves at 300K. The actuators were powered and the influence functions were measured between 35 and 65 K. Even though it is not a functional DM at 35 K, it is a substantial step forward in the development of a cryogenic deformable mirror technology.
机译:Xinetics正在与NASA合作,开发一种低温可变形反射镜(DM),专门针对将来的Origins Program任务(如TPF和JWST)的需求。最重要的是开发在低温下具有电致伸缩性能的电陶瓷材料。本文讨论了349通道离散致动器可变形反射镜演示器的致动器开发测试以及随后的低温可变形反射镜设计和低温测试性能。共点火执行机构的行程响应在35至65 K范围内几乎恒定,因此在150V时执行机构的自由行程约为3微米。 349通道低温DM的设计和制造使用了尽可能少的零件和材料,以最大程度地减少CTE失配。抛光后的镜子在300到35 K的范围内循环两次。在冷却时使用Zygo干涉仪监测rms表面图形,并在两个温度周期内测量一致的数据。该数字从300 K时的0.5波(P-V)变为35 K时的5波,然后恢复为300K的0.6波。致动器已通电,并且在35至65 K之间测量了影响功能。即使它不是35 K时的功能性DM,也仍是低温可变形反射镜技术发展的重要一步。

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