首页> 外文会议>16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference >Fundamental Analysis of a Combined Cycle Hydrocarbon- Liquid Oxygen Tandem Ramjet- Rocket Propulsion System

【24h】

Fundamental Analysis of a Combined Cycle Hydrocarbon- Liquid Oxygen Tandem Ramjet- Rocket Propulsion System

机译：烃-液氧串联冲压发动机-火箭推进系统联合循环的基础分析

获取原文

获取原文并翻译 | 示例

获取外文期刊封面目录资料

页面导航

著录项
引文网络
相似文献
相关主题

著录项

来源
《16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference》|2009年|1-9|共9页
会议地点 Bremen(DE)
作者
R. LeMoyne;
展开▼
作者单位

, Running Springs, CA;

展开▼
会议组织
原文格式 PDF
正文语种 eng
中图分类各类型航空器;
关键词

相似文献

外文文献
中文文献
专利

1. Transient thermal analysis of a cryogenic oxidizer tank in the liquid rocket propulsion system during the prelaunch helium gas pressurization [J] . Kim K.H., Ko H.-J., Kim K., Journal of engineering thermophysics . 2012,第1期

机译：发射前氦气加压期间液体火箭推进系统中低温氧化剂罐的瞬态热分析
2. New Way of Eliminating the Temperature Stratification of Liquid Oxygen in the Tanks of Rocket Propulsion Units [J] . Mitikov YO, Ivanenko IS, Pauk OL Journal of Aeronautics & Aerospace Engineering . 2017,第4期

机译：消除火箭推进器舱内液氧温度分层的新方法
3. Steric Stabilization of Colloidal Aluminium Particles for Advanced Metalized-Liquid Rocket Propulsion Systems [J] . Elbasuney Sherif Combustion, Explosion, and Shock Waves . 2019,第3期

机译：先进金属化 - 液体火箭推进系统的胶体铝颗粒的空间稳定
4. Fundamental Analysis of a Combined Cycle Hydrocarbon- Liquid Oxygen Tandem Ramjet- Rocket Propulsion System [C] . R. LeMoyne American Institute of Aeronautics and Astronautics/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference . 2009

机译：结合循环烃型氧气串联拉力火箭推进系统的根本分析
5. Uncertainty analysis for rocket-based combined cycle (RBCC) systems testing. [D] . Law, Boon-Chuan. 2003

机译：基于火箭的联合循环（RBCC）系统测试的不确定性分析。
6. Thermodynamic Analysis of a Hybrid Power System Combining Kalina Cycle with Liquid Air Energy Storage [O] . Tong Zhang, Xuelin Zhang, Xiaodai Xue, 2019

机译：液体空气储能的混合动力系统混合动力系统的热力学分析
7. Computational Analysis for Rocket-Based Combined-Cycle Systems During Rocket-Only Operation [O] . Yungster S., Steffen C. J. Jr., Smith T. D., 2000

机译：基于火箭的联合循环系统仅火箭运行时的计算分析
8. Liquid Rocket Propulsion - Evolution and Advancements: Rocket-Based Combined Cycle. [R] . Moszee, R. 1999

机译：液体火箭推进 - 演变与进步：基于火箭的联合循环。

获取原文

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

客服微信
服务号