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An improved method for maximizing the payload of electric propulsion spacecraft at low power level

机译：一种在低功率水平下最大化电力推进航天器有效载荷的改进方法

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摘要

Improving payload at low power by reducing total mass of electric propulsion spacecraft

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作者
Zola, C. L.;
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年度 1971
页码 1-16
总页数 16
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ELECTRIC PROPULSION; LAUNCH VEHICLES; OPTIMIZATION; PAYLOAD MASS RATIO; MERCURY SPACECRAFT; ROCKET LAUNCHERS; SOLAR PROPULSION;

机译：电动推进;发射车辆;优化; paYLOaD mass RaTIO; mERCURY spaCECRaFT;火箭发射器;太阳推进;
入库时间 2022-08-29 11:13:28

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1. Maximizing Payload Mass Fractions of Spacecraft for Interplanetary Electric Propulsion Missions [J] . Prashant Patel, Daniel Scheeres, Alec Gallimore Journal of Spacecraft and Rockets . 2006,第4期

机译：最大化用于行星际电动推进任务的航天器的有效载荷质量分数
2. Impact induced compound method for triboelectric-piezoelectric hybrid nanogenerators to achieve Watt level average power in low frequency rotations [J] . Nano Energy . 2020,第期

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3. A Method of Suppressing Fault Currents and Improving the Ground Level Electric Field in a Novel Six-Phase Power Transmission System [J] . Onogi Yukio, Isaka Katsuo, Chiba Atsuo, Power Engineering Review, IEEE . 1983,第4期

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4. Spacecraft Payload Maximization Using Realistic Multi-Mode Models of Electric Propulsion Systems [C] . Vishala Arya, Ehsan Taheri, John Junkins Annual American Control Conference . 2021

机译：使用电动推进系统的现实多模型号的航天器有效载荷最大化
5. Operationally responsive spacecraft using electric propulsion. [D] . Co, Thomas C. 2012

机译：使用电推进的操作响应型航天器。
6. Mini-Generator of Electrical Power Exploiting theMarangoni Flow Inspired Self-Propulsion [O] . Mark Frenkel, Alla Vilk, Irina Legchenkova, 2019

机译：微型发电机组Marangoni流动启发式自我推进
7. Employing Drain-Bias Dependent Electrical Characteristics of Poly-Si TFTs to Improve Gray Level Control in Low Power AMOLED Displays [O] . Xinghua Xu, Botian Huang, Jiali Fan, 2019

机译：采用Poly-Si TFT的漏极偏置依赖性电气特性，以改善低功率AMOLED显示器中的灰度控制
8. An Improved Method for Maximizing the Payload of Electric Propulsion Spacecraft at Low Power Level [R] . Zola, C. L. 1971

机译：一种优化低功率电力推进航天器有效载荷的改进方法

An improved method for maximizing the payload of electric propulsion spacecraft at low power level

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