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Reliability Improvement of Propulsion System in Successful Return- to- Flight of H- 2A Launch Vehicle

机译：H-2A运载火箭成功返航时推进系统的可靠性改进

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《AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit》|2006年|P.1-6|共6页
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作者
I. Igarashi; T. Nakamura; A. Tamura; K. Yoshikawa; Y. Oowada; I. Kubota;
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原文格式 PDF
正文语种
中图分类航空发动机（推进系统）;
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1. Propulsion vehicle integration for reusable launcher using in-flight oxygen collection [J] . D. Bizzarri, P. Hendrick, G. Heyen, Aerospace science and technology . 2008,第6期

机译：使用飞行中的氧气收集装置，将推进器与可重复使用的发射器集成在一起
2. Designing Propulsion reliability of space Launch vehicles [J] . Subir Ghosh Quality engineering . 1999,第3期

机译：设计太空运载火箭的推进可靠性
3. Aerojet's AJ26 Flight Engine Delivers Successful Hot-Fire Test for Orbital's Taurus II Space Launch Vehicle [J] . Energy Business Journal . 2011,第jana3aocta31期

机译：Aerojet的AJ26飞行引擎为Orbital的Taurus II太空运载火箭成功进行了热火测试
4. Reliability Improvement of Propulsion System in Successful Return- to- Flight of H- 2A Launch Vehicle [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/Society of Automotive Engineers/American Society for Engineering Education Joint Propulsion Conference Exhibit . 2006

机译：在成功返回到飞行中的推进系统的可靠性改进 - 2A发射车辆
5. Interactions between Flight Dynamics and Propulsion Systems of Air-Breathing Hypersonic Vehicles. [D] . Dalle, Derek J. 2013

机译：带空气呼吸的超音速飞行器的飞行动力学与推进系统之间的相互作用。
6. Local Observability Analysis of Star Sensor Installation Errors in a SINS/CNS Integration System for Near-Earth Flight Vehicles [O] . Yanqiang Yang, Chunxi Zhang, Jiazhen Lu 2017

机译：近地飞行器SINS / CNS集成系统中恒星传感器安装错误的局部可观察性分析
7. Development and Flight Results of Solid Propulsion System for Enhanced Epsilon Launch Vehicle [O] . Koki KITAGAWA, Shinichiro TOKUDOME, Keiichi HORI, 2019

机译：增强普通发动车辆固体推进系统的开发和飞行结果
8. Reliability, Maintainability, and Availability: Consideration During the Design Phase in Ground Systems to Ensure Successful Launch Support. [R] . Gillespie, A. M. 2012

机译：可靠性，可维护性和可用性：在地面系统设计阶段考虑确保成功的发射支持。

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