IN-SPACE CHEMICAL PROPULSION SYSTEM MODEL

机译：空间化学推进系统模型

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Multiple, new technologies for chemical systems are becoming available and include high temperature rockets, very light propellant tanks and structures, new bipropellant and monopropellant options, lower mass propellant control components, and zero boil off subsystems. Such technologies offer promise of increasing the performance of in-space chemical propulsion for energetic space missions. A mass model for pressure-fed, Earth and space-storable, advanced chemical propulsion systems (ACPS) was developed in support of the NASA MSFC In-Space Propulsion Program. Data from flight systems and studies defined baseline system architectures and subsystems and analyses were formulated for parametric scaling relationships for all ACPS subsystems. The paper will first provide summary descriptions of the approaches used for the systems and the subsystems and then present selected analyses to illustrate use of the model for missions with characteristics of current interest.

机译：化学系统有多种新技术可供使用，包括高温火箭，极轻的推进剂储罐和结构，新的双推进剂和单推进剂选项，较低质量的推进剂控制组件以及零蒸发子系统。此类技术为提高高能太空飞行的空间化学推进性能提供了希望。为支持美国国家航空航天局MSFC太空推进计划，开发了一种压力馈送的，可在地面和空间存储的先进化学推进系统（ACPS）的质量模型。来自飞行系统和研究的数据定义了基线系统架构和子系统，并为所有ACPS子系统的参数比例关系制定了分析。本文将首先提供用于系统和子系统的方法的摘要说明，然后介绍选定的分析，以说明该模型用于具有当前关注特征的任务的用途。

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来源
《4th International spacecraft propulsion conference》|2004年|p.1-6|共6页
会议地点 Sardinia(IT)
作者
David C. Byers; Gordon Woodcock; M. P. J.Benfield;
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作者单位

SAIC, 4465 Pacific CoastHwy, Torrance, CA 90505 USA,byersdc@ aol. com;

Cray Research, 655 Discovery Drive, Suite 300, Huntsville, AL 35806 USA, grw33@comcast.net;

SAIC, 675 Discovery Drive, Suite 300, Huntsville, AL 35806,michael.pj.benfzeld@saic.com;

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原文格式 PDF
正文语种 eng
中图分类推进系统（发动机、推进器）;
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机译：高温高压激光化学气相沉积法在核热推进和空间制造中的高温纳米复合材料
2. COMPUTATIONALLY BASED DEVELOPMENT OF CHEMICAL KINETICS MECHANISMS FOR MODELING THE COMBUSTION CHAMBER DYNAMICS OF ROCKET PROPULSION SYSTEMS [J] . Michael J. McQuaid, Chiung-Chu Chen, Anthony J. Kotlar, International journal of energetic materials and chemical propulsion . 2013,第1期

机译：基于计算的火箭推进系统燃烧室动力学模型动力学机理的开发
3. Optimization of In-Space Supply Chain Design Using High-Thrust and Low-Thrust Propulsion Technologies [J] . Jagannatha Bindu B., Ho Koki Journal of Spacecraft and Rockets . 2018,第3期

机译：利用高推力和低推力推进技术优化空间供应链设计
4. IN-SPACE CHEMICAL PROPULSION SYSTEM MODEL [C] . David C. Byers, Gordon Woodcock, M. P. J.Benfield International spacecraft propulsion conference . 2004

机译：空间内化学推进系统模型
5. Non-Potential Magnetic Fields and Magnetic Reconnection In Low Collisional Plasmas-Discovery of Solar EUV Mini-Sigmoids and Development of Novel In-Space Propulsion Systems. [D] . Chesny, David. 2013

机译：低碰撞等离子体中的非势能磁场和磁重连接-太阳EUV微型乙状结肠的发现和新型空间推进系统的开发。
6. Self-propulsion and interactions of catalytic particles in a chemically active medium [O] . Edward J. Banigan, John F. Marko -1

机译：在化学活性介质中催化颗粒的自推进和相互作用
7. In-Space Propulsion Assessment Processes and Criteria for Affordable Systems [O] . Rhodes Russel, Zapata Edgar 1999

机译：经济适用系统的空间推进评估程序和标准
8. In-Space Chemical Propulsion System Model [R] . Byers, David C., Woodcock, Gordon, Benfield, Michael P. J. 2004

机译：空间化学推进系统模型

IN-SPACE CHEMICAL PROPULSION SYSTEM MODEL

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