首页> 外文会议>The Twenty-Second International Symposium on Space Technology and Science , May 28 - Jun 4, 2000, Morioka >Development and Firing Tests of Experimental Thruster for Space Vehicle Using NUSK-CMC
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Development and Firing Tests of Experimental Thruster for Space Vehicle Using NUSK-CMC

机译:基于NUSK-CMC的航天器实验推进器的研制与射击试验。

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摘要

A ceramic matrix composite (CMC) system, designated as NUSK-CMC has been developed by NAL, Ube Industries Ltd., Shikibo Ltd., and Kawasaki Heavy Industries Ltd. using Si-Ti-C-O (Tyranno~R) fiber, 3-D fabrics reinforcement, PIP matrix and glass seal technologies. By cooperation of these four sectors, static strength level has been upgraded to 380 MPa in high temperature air up to 1200°C in this decade. A research and development program was planned for establishing application technology of CMC to space vehicle components and a chosen component was a combustion chamberozzle of an experimental thruster. Brief overview of R & D program is given here as well as lessons learned by this activity.
机译:NAL,宇部兴产株式会社,志宝株式会社和川崎重工株式会社开发了一种名为NUSK-CMC的陶瓷基复合材料(CMC)系统,该系统使用Si-Ti-CO(Tyranno〜R)纤维3- D织物增强,PIP基体和玻璃密封技术。通过这四个领域的合作,在此十年中,在高达1200°C的高温空气中,静强度等级已提高到380 MPa。计划制定一项研究和开发计划,以建立CMC在航天器部件上的应用技术,选择的部件是实验推进器的燃烧室/喷嘴。这里给出了R&D计划的简要概述,以及从此活动中学到的经验教训。

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