气动增压空间推进系统及相关技术试验研究

摘要

The scheme and composition of the pneumatic pressurization space propulsion system are introduced. Experimental study on the new pneumatic pressurization liquid rocket engine technolo-gy is carried out. The test results and system performance related to the pneumatic pressurization space propulsion are analyzed emphatically. The results show that the pneumatic pressurization space propulsion system has the advantages of multiple start and high chamber pressure. The correlation technology was verified.%简要介绍了气动增压空间推进系统方案及组成,开展了基于气动增压原理的新型发动机技术试验研究,重点分析了气动增压空间推进相关技术试验结果和系统性能.结果表明,气动增压空间推进系统同时具备多次起动和高室压的优点,相关技术得到了验证.