Low power - high payload launch spacecraft with low inertial acceleration in deep space

• 1. 低深宽比的单质量块三轴MEMS惯性加速度计及其制备方法 [P] . 中国专利： CN111289772A . 2020-06-16
• 2. 具有低功率、高写反应时间模式和高功率、低写反应时间模式和／或可独立选择的写反应时间的存储器件和方法 [P] . 中国专利： CN1748261A . 2006-03-15
• 3. Low power - high payload launch spacecraft with low inertial acceleration in deep space [P] . 英国专利： GB201700455D0 . 2017-02-22

  机译： 低功率-高载荷发射航天器，在深空具有低惯性加速度

• 4. A spacecraft with a pillar for forming a stack, a stack with at least two such spacecraft installed on the launcher, and a method for lowering the spacecraft [P] . 日本专利： JP6448855B2 . 2019-01-09

  机译： 一种具有用于形成堆的支柱的航天器，在发射器上安装至少两个这样的航天器的堆以及降低航天器的方法

• 5. Passive isolation devices providing low frequency damping of low mass payloads and spacecraft isolation systems employing the same [P] . 欧洲知识产权局专利： EP2607240A2 . 2013-06-26

  机译： 可对低频有效载荷进行低频衰减的无源隔离装置以及采用该隔离装置的航天器隔离系统

• 1. A Precision-Positioning Method for a High-Acceleration Low-Load Mechanism Based on Optimal Spatial and Temporal Distribution of Inertial Energy [J] . Xin Chen, Youdun Bai, Zhijun Yang, 工程科学（英文版） . 2015,第003期
• 2. A Precision-Positioning Method for a High-Acceleration Low-Load Mechanism Based on Optimal Spatial and Temporal Distribution of Inertial Energy [J] . Xin Chen, Youdun Bai, Zhijun Yang, 工程（英文） . 2015,第003期
• 3. Particle-in-Cell Simulation Study on the Floating Potential of Spacecraft in the Low Earth Orbit [J] . TANG Daotan, YANG Shengsheng, ZHENG Kuohai, 等离子体科学和技术（英文版） . 2015,第004期
• 4. Development of low-coherence high-power laser drivers for inertial confinement fusion [J] . Yanqi Gao, Jiani Liu, Haitao Shi, 极端条件下的物质与辐射（英文） . 2020,第006期
• 5. Formation control for networked spacecraft in deep space [J] . Wang Nan, Jin Rui, Xu Jieqiong 高技术通讯（英文版） . 2011,第004期
• 6. First results from the LUCID-Timepix spacecraft payload onboard the TechDemoSat-1 satellite in Low Earth Orbit [J] . Furnell Will, Shenoy Abhishek, Fox Elliot, Advances in space research . 2019,第5期
• 7. Solar X-ray Spectrometer (Soxs) Mission on Board GSAT2 Indian Spacecraft: The Low-Energy Payload [J] . Rajmal Jain, Hemant Dave, A. B. Shah, Solar Physics . 2005,第1期
• 8. Solar x-ray Spectrometer (SOXS) mission on board GSAT2 Indian spacecraft: The low-energy payload [J] . Jain R, Dave H, Shah AB, Solar physics . 2005,第1期
• 9. Compact Inertial triaxial monolithic sensors for low-frequency acceleration measurement of spacecrafts and satellites [C] . F. Barone, G. Giordano, F. Acernese, Conference on sensors, systems, and next-generation satellites . 2018
• 10. Minimum fuel trajectories for low-thrust power-limited spacecraft. [D] . Golan, Oded M. 1990
• 11. Prokaryotic and Fungal Characterization of the Facilities Used to Assemble Test and Launch the OSIRIS-REx Spacecraft [O] . Aaron B. Regberg, Christian L. Castro, Harold C. Connolly Jr., 2020
• 12. Unification of filling station equipment intented for filling of spacecraft, upper stages and low-thrust propulsion systems of space launch systems [O] . Геннадий Леонидович Поздеев, Виктор Петрович Фролов 2017
• 13. An Improved Method for Maximizing the Payload of Electric Propulsion Spacecraft at Low Power Level [R] . Zola, C. L. 1971

• 1. 低循环载荷叠加高频低幅载荷对疲劳短裂纹生成的初始寿命之影响 [C] . 李俊 . 中国航空学会飞机、发动机疲劳寿命学术讨论会 . 1986
• 2. 深空光通信高速率、高功率激光发射技术的研究 [A] . 曹青 . 2012