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RESEARCH PROGRESSES ON GREEN PROPULSION TECHNOLOGY FOR HAN-BASED PROPELLANT

机译:汉族推进剂绿色推进技术研究进展

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In the area of liquid monopropellant propulsion system, the goal of replacing current highly toxic and easily flammable propellant hydrazine by liquid Hydroxylammonium Nitrate (HAN)—based propellants has drawn the attentions of the relevant industry worldwide. Shanghai Institute of Space Propulsion (SISP) has been focusing on the novel technology since the late 1990s and developing a thrustcr using HAN-based propellant. The primary objective of using HAN-based propellant is to reduce operational hazards and simplify the propellant transportation and storage compared with the conventional propellant hydrazine. The monopropellant developed by SISP has the same theoretical specific impulse as hydrazine and provides 30% density specific impulse improvement over hydrazine. This paper summarizes the ongoing work and several achievements based on the HAN propellant and related rocket engine technologies. Firstly, more than 20 experimental HAN thrusters have been built and tested in vacuum level, the results from firing tests of these thrusters are presented in the paper, and the Engineering Model of 60-Xewton thruster (EM-60) has now achieved more than 1200s accumulated firing time, 1000 pulses and 100s longest continuous firing time with a catalyst bed temperature preheated to 120 degree. It delivers a specific impulse performance of approximately 220s (with 50:1 expansion ratio nozzle) and the highest temperature of the thruster obtained is no more than 1200 degree during thruster operations. Results from the firing tests have validated the thruster design, specific impulse, combustion stability, short pulse capability, and blow-down capability. Secondly, the propellant has been stored for more than 2 years and initial material compatibility screening and testing has also been finished. The current status shows that the HAN propulsion Technology Readiness Level (TRL) 5 has been reached. SISP is preparing a flight program for demonstrating this novel propulsion technology and towards qualified products for space applications in future.
机译:在液体单推进剂推进系统领域,以液态硝酸羟铵(HAN)为基础的液体推进剂替代目前剧毒且易燃的推进剂肼的目标引起了全世界相关行业的关注。自1990年代后期以来,上海太空推进研究所(SISP)就一直致力于新技术的研究,并使用基于HAN的推进剂开发了推力发动机。与传统的推进剂肼相比,使用基于HAN的推进剂的主要目的是减少操作危险并简化推进剂的运输和储存。 SISP开发的单推进剂具有与肼相同的理论比冲量,比肼具有30%的密度比冲量提高。本文总结了基于HAN推进剂和相关火箭发动机技术的正在进行的工作和取得的一些成就。首先,已经制造了20多台HAN推进器实验装置并在真空水平下进行了测试,这些推进器的点火测试结果已在本文中进行了介绍,而60 Xewton推进器(EM-60)的工程模型现在已经达到了催化剂床温预热至120度,累计燃烧时间为1200s,脉冲数为1000,最长连续燃烧时间为100s。它具有约220s的特定脉冲性能(使用50:1的膨胀比喷嘴),并且在推进器运行期间获得的推进器最高温度不超过1200度。点火测试的结果验证了推进器的设计,比脉冲,燃烧稳定性,短脉冲能力和排污能力。其次,推进剂已经保存了2年以上,初步的材料相容性筛选和测试也已经完成。当前状态表明已达到HAN推进技术准备水平(TRL)5。 SISP正在准备一个飞行计划,以展示这种新颖的推进技术,并在未来向太空应用领域寻求合格的产品。

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