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| 一种新型双组元卫星推进剂的研究 | |
| 引用本文： | 黄继庆,鲍世国,刘汉林,刘江强. 一种新型双组元卫星推进剂的研究[J]. 火箭推进, 2013, 39(3): 87-92 |
| 作者姓名： | 黄继庆 鲍世国 刘汉林 刘江强 |
| 作者单位： | 北京航天试验技术研究所,北京,100074 |
| 基金项目： | 中国航天科技集团公司支撑项目 |
| 摘 要： | 通过热力学计算,选择NHO-3作为甲基肼高能添加剂,通过冰点测试、着火延迟期测试确定了NHO-3的含量,该种以甲基肼为主体的新型燃料与氧化剂MON-20组成的双组元推进剂具有冰点低、比冲高、着火延迟期短的优点,可应用于卫星、飞船等领域。 |
| 关 键 词： | 高能添加剂 高比冲 低冰点 着火延迟 |
Research on a novel bipropellant for spacecrafts |
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| HUANG Ji-qing , BAO Shi-guo , LIU Han-lin , LIU Jiang-qiang. Research on a novel bipropellant for spacecrafts[J]. Journal of Rocket Propulsion, 2013, 39(3): 87-92 | |
| Authors: | HUANG Ji-qing BAO Shi-guo LIU Han-lin LIU Jiang-qiang |
| Affiliation: | (Beijing Institute of Aerospace Testing Technology,Beijing 100074,China) |
| Abstract: | NHO-3 was selected as the high energetic additive of methylhydrazine via thermodynamic calculation.The content of NHO-3 was confirmed via freezing point test and ignition delay test.The bipropellant consisting of oxidant MON-20 and the novel propellant,in which methylhydrazine was taken as the main part,has the advantages of low freezing point,high specific impulse and short ignition delay.It may be applied to satellite,spaceship,etc. |
| Keywords: | high energetic additive high specific impulse low freezing point ignition delay |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |