Reusable launch vehicle development research

机译：可重复使用的运载火箭发展研究

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NASA has generated a program approach for a SSTO reusable launch vehicle technology (RLV) development which includes a follow-on to the Ballistic Missile Defense Organization's (BMDO) successful DC-X program, the DC-XA (Advanced). Also, a separate sub-scale flight demonstrator, designated the X-33, will be built and flight tested along with numerous ground based technologies programs. For this to be a successful effort, a balance between technical, schedule, and budgetary risks must be attained. The adoption of BMDO's 'fast track' management practices will be a key element in the eventual success of NASA's effort.

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年度 1995
页码 1-47
总页数 47
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
BALLISTIC MISSILES; MISSILE DEFENSE; NASA SPACE PROGRAMS; REUSABLE LAUNCH VEHICLES; SINGLE STAGE TO ORBIT VEHICLES; PROVING; RESEARCH AND DEVELOPMENT; RISK; SCHEDULES; TECHNOLOGY ASSESSMENT;

机译：BaLLIsTIC mIssILEs;导弹防御;美国宇航局太空计划;可重复使用的发射车辆;轨道车辆的单一阶段;验算;研究与开发;风险;时间表;技术评估;

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1. Development of large-sized Titanium alloy Ti6Al4V and nickel-based superalloy Inconel-718 forgings for Reusable Launch Vehicle-Technology Demonstrator flight [J] . Gupta R. K., Kumar V. Anil, Ramkumar P., Current Science: A Fortnightly Journal of Research . 2018,第1期

机译：大型钛合金Ti6Al4V和基于镍的超合金Inconel-718锻件的开发可重复使用的发射车辆技术演示飞行
2. DESIGN, DEVELOPMENT AND QUALIFICATION OF CARBON-CARBON NOSE CAP FOR REUSABLE LAUNCH VEHICLE APPLICATION [J] . Prakhar Agarwal, S. Mahendran, Abhijeet Rathore, Journal of Aerospace Sciences and Technologies . 2017,第3a期

机译：可重复使用发射车辆的碳鼻帽的设计，开发和鉴定
3. DESIGN AND DEVELOPMENT OF ATTITUDE CONTROL SYSTEMS FOR REUSABLE LAUNCH VEHICLE [J] . Lala Surya Prakash, G. C. Arun, Biswaroop Sarkar, Journal of Aerospace Sciences and Technologies . 2017,第3a期

机译：可重复使用发射车辆姿态控制系统的设计与开发
4. Relying on Telemetry for Mission Critical Decisions: Lessons Learned from NASA' Reusable Launch Vehicle for use on the Air Force's Next Generation Reusable Launch Vehicle [C] . Len Losik Annual International Telemetering Conference and Technical Exhibition . 2012

机译：依靠遥测的关键项任务批判性决策：从美国宇航局的可重复使用的发动机使用的经验教训用于空军的下一代可重复使用的发射车辆
5. Development of a finite difference neighboring optimal control law and application to the optimal landing of a reusable launch vehicle. [D] . Wetzel, Todd Andrew. 1996

机译：有限差邻近最优控制律的发展及其在可重复使用运载火箭最优着陆中的应用。
6. Research on the Rapid and Accurate Positioning and Orientation Approach for Land Missile-Launching Vehicle [O] . Kui Li, Lei Wang, Yanhong Lv, 2015

机译：陆空导弹发射车快速准确的定位定向方法研究
7. Relying on Telemetry for Mission Critical Decisions: Lessons Learned from NASA's Reusable Launch Vehicle for Use on the Air Force's Next Generation Reusable Launch Vehicle [O] . Losik Len 2012

机译：依靠遥测完成关键任务决策：从美国宇航局可重复使用运载火箭中学到的教训，可用于空军的下一代可重复使用运载火箭
8. A Method of Integrating Aeroheating into Conceptual Reusable Launch Vehicle Design: Evaluation of Advanced Thermal Protection Techniques for Future Reusable Launch Vehicles [R] . Olds, John R., Cowart, Kris 2001

机译：将航空加热与概念性可重复使用运载火箭设计相结合的方法：评估未来可重复使用运载火箭的先进热保护技术

Reusable launch vehicle development research

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