Study on Ceramic Thruster
Study on Ceramic Thruster
批准号:
14205141
负责人:
UESUGI Kuninori
金额:
$34.44万
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (A)
财政年份:
2002
资助国家:
日本
项目状态:
已结题
起止时间:
2002 至 2005
中文摘要
陶瓷材料具有优异的耐热性能,是航天器星载推进器最有前途的材料之一。然而,它们是易碎的,因此到目前为止还没有在真正的飞行任务中使用。它可能由于发射时的机械振动、发射时的热冲击或空间碎片的碰撞而破裂。研制了一种由硅基单片陶瓷制成的500N级双组元推进器。作为研制的第一步,将现有金属推进器的燃烧室和喷管更换为陶瓷,并进行了包括机械振动试验、点火试验和冲击试验在内的一系列合格试验。试验结果验证了该方案在热震和发射环境下的可行性,喷油器模块的设计没有对常规版本进行修改。这意味着性能的改善是不可预期的,因为喷射器的设计是决定推进剂如何燃烧、推进器如何变热的关键。这意味着通过允许更高的燃烧室温度来改善性能的可能性。到目前为止,本研究主要集中在实现陶瓷基推进器,而不是考虑性能。研制成功了性能与常规陶瓷推力器相当的陶瓷推力器。
英文摘要
Ceramics are one of the most promising materials for the spacecraft on-board thrusters because of their superior performance on heat resistance. However they are brittle, and thus they have not been used in the real flight missions so far. It might be fractured due to mechanical vibration at launch, thermal shock at firing, or by collision of space debris. We have developed a 500N class bipropellant thruster made of Si-based monolithic ceramic. As a first step of the development, the chamber and nozzle of the existing metallic thruster were replaced to ceramics, and have conducted a series of qualification tests including mechanical vibration tests, firing tests and impact test. Test results confirmed its feasibility in accordance with the thermal shock and launch environment.Momentarily, the design of the injector block is not revised from the conventional version. It means that the improvement of the performance is not expected, because the design of the injector is the key point to decide how the propellant combusts, and how the thruster becomes hot. It implies the possibility of improving the performance by allowing a higher chamber temperature.So far, this study has concentrated to realize the ceramic based thruster, without concerning the performance. As a result, the authors have successfully developed the ceramic thruster which has similar performance to the conventional ones.
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Ceramic Thruster for Satellites-High Reliability Design of Ceramic Component,
卫星用陶瓷推进器——陶瓷部件的高可靠性设计,
DOI:
--
发表时间:
2005
期刊:
Materia 44 (7)
影响因子:
--
作者:
[Y.Nonaka, K.Morishima, H.Mishima, K.Furukawa, E.Sato, S.Sawai, K.T.Uesugi]
通讯作者:
K.T.Uesugi
衛星用セラミックススラスタ-セラミックス部材の高信頼性設計
卫星用陶瓷推进器——陶瓷部件的高可靠性设计
DOI:
--
发表时间:
2005
期刊:
まてりあ 第44巻・第7号
影响因子:
--
作者:
[野中吉紀, 森島克成, 三島弘行, 古川克己, 佐藤英一, 澤井秀次郎, 上杉邦憲]
通讯作者:
上杉邦憲
Development of Ceramic Thruster for Spacecraft Propulsion System
航天器推进系统陶瓷推进器的研制
DOI:
--
发表时间:
2004
期刊:
4^<th> International Spacecraft Propulsion Conference 2-9
影响因子:
--
作者:
[K.Takita, K.Hisatsune, Y.Nonaka, H.Mishima, K.T.Uesugi, E.Sato, S.Sawai]
通讯作者:
S.Sawai
Development of Monolithic Ceramic Thruster for Interplanetary Exploration,
用于星际探索的整体陶瓷推进器的开发,
DOI:
--
发表时间:
2005
期刊:
Proceedings of sixth IAA International Conference on Low-Cost Planetary Missions
影响因子:
--
作者:
[K.T.Uesugi, E.Sato, S.Sawai, K.Furukawa, H.Mishima, K.Morishima, Y.Nonaka, M.Kondo]
通讯作者:
M.Kondo
惑星探査機用セラミックススラスタの開発
行星探测器陶瓷推进器的开发
DOI:
--
发表时间:
2005
期刊:
第21回宇宙構造・材料シンポジウム公園集
影响因子:
--
作者:
[佐藤英一, 澤井秀次郎, 上杉邦憲, 野中吉紀, 森島克成, 三島弘行, 古川克己]
通讯作者:
古川克己
共 21 条
Research for Improvement of Performance of Bi-propellant Thruster through Numerical Flow Analysis
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批准号:19569007
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$2.46万
-
财政年份:2007
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负责人:UESUGI Kuninori
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依托单位:
海外基金