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Conceptual design and performance of large propulsion stages dry launched within a 50K space shuttle payload compartment

机译：大型推进级的概念设计和性能在50K航天飞机有效载荷舱内干式发射

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作者
Kiersarsky, A. S.; Skeer, M. H.;
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年度 1969
页码 1-32
总页数 32
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
SPACE LOGISTICS; SPACE SHUTTLES; SPACECRAFT DESIGN; CONFIGURATION MANAGEMENT; ENGINEERING DRAWINGS; EQUIPMENT SPECIFICATIONS; PAYLOADS; SYSTEMS ENGINEERING; TABLES (DATA);

机译：空间物流;太空沙滩;航天器设计;配置管理;工程图纸;设备规格;有效载荷;系统工程;表（数据）;

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机译：一种多目标，多学科的设计优化方法，用于航天器双推进系统的概念设计
2. Conceptual Design of Single-Stage Launch Vehicle with Hybrid Rocket Engine for Scientific Observation Using Design Informatics [J] . Kazuhisa CHIBA, Masahiro KANAZAKI, Masaki NAKAMIYA, Journal of Space Engineering . 2013,第1期

机译：使用设计信息学的混合火箭发动机单级运载火箭概念设计
3. Attached payloads on spacehab, growign from the space shuttle to the space station [J] . Kenneth a.Jackson, Sr.Michael G.Jacox, Dr.Carlo Mirra Acta astronautica . 2001,第5a12期

机译：从航天飞机到空间站的附着在太空舱上的有效载荷
4. SIMULATION, DEVELOPMENT, AND FIELD MEASUREMENT VALIDATION OF AN ISOLATION SYSTEM FOR A NEW ELECTRONICS CABINET IN THE SPACE SHUTTLE LAUNCH ENVIRONMENT WITHIN THE MOBILE LAUNCH PLATFORM [C] . Alan R. Klembczyk, Michael W. Mosher Shock and Vibration Symposium . 2007

机译：在移动发射平台内的空间班车发射环境中新电子柜的隔离系统的仿真，开发和现场测量验证
5. Propulsion enhancement contributions to the performance of space launch vehicles. [D] . Edwards, Russell H. 2007

机译：推进力增强对空间运载火箭的性能有贡献。
6. Investigation of Design Space for Freeze-Drying: Use of Modeling for Primary Drying Segment of a Freeze-Drying Cycle [O] . Venkat Rao Koganti, Evgenyi Y. Shalaev, Mark R. Berry, 2011

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7. Data Relay System for Space Shuttle and Payload Pre-Launch Checkout [O] . ODonnell Hugh B., Wise Thomas E., Ngo David Q. 1987

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Conceptual design and performance of large propulsion stages dry launched within a 50K space shuttle payload compartment

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