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Propellant selection for unmanned spacecraft propulsion systems. Volume 3 - Study of propulsion stage commonality and attitude control systems requirements, phase 2 Final report

机译：无人航天器推进系统的推进剂选择。第3卷 - 推进阶段共性和姿态控制系统要求的研究，第2阶段最终报告

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Feasibility of common stage for alternate space missions and attitude control systems for unmanned spacecraft propulsion system

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年度 1969
页码 1-301
总页数 301
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ATTITUDE CONTROL; FEASIBILITY; PERFORMANCE PREDICTION; SPACECRAFT PROPULSION; UNMANNED SPACECRAFT; PROPULSION SYSTEM PERFORMANCE; SPACE MISSIONS;

机译：态度控制;可行性;绩效预测;航天器推进; UNmaNNED spaCECRaFT;推进系统性能;空间使命;

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1. 航天器推进剂晃动与控制系统之间耦合效应的混合型估算方法 [J] . 齐乃明, 董锴, 李运迁, 南京航空航天大学学报（英文版） . 2009,第002期
2. Sustainer electric propulsion system application for spacecraft attitude control [J] . V.A. Obukhov, A.I. Pokryshkin, G.A. Popov, Acta astronautica . 2010,第1a2期

机译：增速器电力推进系统在航天器姿态控制中的应用
3. 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
4. Attitude-Orbit Cooperative Control for Small-Scale Spacecraft with Chemical Propulsion: Adaptive Sliding Mode Control Based on Neural Network [J] . Wang Guogang, Liu Keping, Sun Zhongbo, Journal of aerospace engineering . 2020,第6期

机译：具有化学推进的小型航天器的态度轨道协作控制：基于神经网络的自适应滑模控制
5. THERMODYNAMICS-BASED MATERIALS SELECTION FOR CORROSION-RESISTANT PERFORMANCE IN HIGH-TEMPERATURE MISSILE PROPULSION SYSTEMS. PART I. CONSIDERATION OF CONDENSED PHASE EQUILIBRIA [C] . Mark M. Opeka ECS Meeting . 2005

机译：高温导弹推进系统中耐腐蚀性能的热力学基础材料。第一部分。考虑凝结相平衡
6. A numerical and experimental study of a two-stage microwave electrothermal thruster for spacecraft propulsion. [D] . Chiravalle, Vincent Patrick. 2003

机译：用于航天器推进的两级微波电热推进器的数值和实验研究。
7. Supervising and Controlling Unmanned Systems: A Multi-Phase Study with Subject Matter Experts [O] . Talya Porat, Tal Oron-Gilad, Michal Rottem-Hovev, -1

机译：监督和控制无人系统：主题专家的多阶段研究
8. Conceptual Design of Cold Gas Propulsion System of a Ground Simulator for Maneuver and Attitude Control Design Verification of Spacecraft [O] . Jae-Hoon Kim, Kyun Ho Lee, Sung Kyung Hong, 2015

机译：用于操纵和姿态控制的地面模拟器冷气推进系统的概念设计宇宙飞船的设计验证
9. Propellant Selection for Unmanned Spacecraft Propulsion Systems. Volume 3 - Study of Propulsion Stage Commonality and Attitude Control Systems Requirements, Phase 2 Final Report [R] . 1969

机译：无人航天器推进系统的推进剂选择。第3卷 - 推进阶段通用性和姿态控制系统要求研究，第2阶段最终报告

Propellant selection for unmanned spacecraft propulsion systems. Volume 3 - Study of propulsion stage commonality and attitude control systems requirements, phase 2 Final report

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