首页> 美国政府科技报告 >VOYAGER SPACECRAFT SYSTEM. VOLUME C - ALTERNATE DESIGNS CONSIDERED FOR SPACECRAFT PROPULSION SYSTEMS FINAL TECHNICAL REPORT, TASK B

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VOYAGER SPACECRAFT SYSTEM. VOLUME C - ALTERNATE DESIGNS CONSIDERED FOR SPACECRAFT PROPULSION SYSTEMS FINAL TECHNICAL REPORT, TASK B

机译：VOYaGER航天器系统。第C卷 - 为航天器推进系统考虑的替代设计最终技术报告，任务B

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SOLID-LIQUID SYSTEMS SIZED FOR 1971 AND 1973 MISSIONS AND 1975 AND 1977 MISSIONS, APOLLO LUNAR EXCURSION MODULE DESCENT PROPULSION SYSTEM, AND TITAN III-C TRANSTAGE

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年度 1966
页码 1-234
总页数 234
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
APOLLO PROJECT; DESCENT PROPULSION SYSTEMS; LUNAR MODULE; PROPELLANTS; PROPULSION; PROPULSION SYSTEM CONFIGURATIONS; PROPULSION SYSTEM PERFORMANCE; SOLID PROPELLANTS; SPACE MISSIONS; SPACECRAFT PROPULSION; TITAN; TITAN LAUNCH VEHICLES; VOYAGER PROJECT; LIQUID PROPELLANT; LUNAR EXCURSION MODULE /LEM/; PROPULSION SYSTEM; SOLID PROPELLANT; SPACE MISSION; TITAN LAUNCH VEHICLE; VOYAGER PROJECT;

机译：apOLLO项目;下降推进系统;登月舱;推进剂;推进;推进系统配置;推进系统性能;固体推进剂;空间使命;航天器推进; TITaN; TITaN推出车辆; VOYaGER pROJECT;液体推进剂; LUNaR EXCURsION mODULE / LEm /;推进系统;固体推进剂;空间使命; TITaN推出车辆; VOYaGER pROJECT;

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专利

1. Ed Stone has spent 36 years guiding the twin Voyager spacecraft through the Solar System. Next stop, interstellar space. [J] . ALEXANDRA WITZE Nature . 2013,第7450期

机译：埃德·斯通（Ed Stone）已花了36年的时间来引导双旅行者号飞船通过太阳系。下一站，星际空间。
2. A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system [J] . Fazeley H. R., Taei H., Naseh H., Structural and multidisciplinary optimization . 2016,第1期

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
3. Joint Optimization of Control and Main Trajectory and Design Parameters of an Interplanetary Spacecraft with an Electric Propulsion System [J] . Petukhov V. G., Ivanyukhin A. V., Wook Woo Sang Cosmic research . 2019,第3期

机译：带有电动推进系统的行星际航天器的控制，主要轨迹和设计参数的联合优化
4. Analysis for Feasibility of Spitzer's Schemes Complication for Spacecraft Final Insertion into Geostationary Orbit by Electric Propulsion [C] . Mikhail Konstantinov, Victoria Svotina Russian-German conference on electric propulsions and their application . 2017

机译：Spitzer's SubseS与电动推进轨道地球静止轨道复杂化的可行性分析
5. Variable Structure Feedback Control with Application to Spacecraft with Small Thrust Propulsion Systems [D] . Kitchen-McKinley, Samuel J. 2017

机译：变结构反馈控制在小推力航天器中的应用
6. A technical evaluation of the Nucletron FIRST system: Conformance of a remote afterloading brachytherapy seed implantation system to manufacturer specifications and AAPM Task Group report recommendations [O] . Mark J. Rivard, Dee‐Ann Radford Evans, Ian Kay 2005

机译：Nucletron FIRST系统的技术评估：远程后载近距离放射治疗植入系统符合制造商规范和AAPM任务组报告的建议
7. Dynamic Isotope Power System (DIPS) Applications Study. Volume II. Nuclear Integrated Multimission Spacecraft (NIMS) design definition. Final report [O] . W. Z. Prickett 1979

机译：动态同位素电力系统（DIPS）应用研究。第II卷。核综合多次航天器（NIMS）设计定义。总结报告

VOYAGER SPACECRAFT SYSTEM. VOLUME C - ALTERNATE DESIGNS CONSIDERED FOR SPACECRAFT PROPULSION SYSTEMS FINAL TECHNICAL REPORT, TASK B

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