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Space Shuttle with rail system and aft thrust structure securing solid rocket boosters to external tank

机译：带有轨道系统和后部推力结构的航天飞机将固体火箭助推器固定在外部油箱上

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The configuration and relationship of the external propellant tank and solid rocket boosters of space transportation systems such as the space shuttle are described. The space shuttle system with the improved propellant tank is shown. The external tank has a forward pressure vessel for liquid hydrogen and an aft pressure vessel for liquid oxygen. The solid rocket boosters are joined together by a thrust frame which extends across and behind the external tank. The thrust of the orbiter's main rocket engines are transmitted to the aft portion of the external tank and the thrust of the solid rocket boosters are transmitted to the aft end of the external tank.

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年度 1984
页码 1-10
总页数 10
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
BOOSTER ROCKET ENGINES; EXTERNAL TANKS; PRESSURE VESSELS; PROPELLANT TANKS; SOLID PROPELLANT ROCKET ENGINES; SPACE SHUTTLE BOOSTERS; SPACE SHUTTLE ORBITERS; SPACECRAFT CONFIGURATIONS; LIQUID HYDROGEN; LIQUID OXYGEN; SPACE SHUTTLE PAYLOADS;

机译：BOOsTER ROCKET ENGINEs;外部坦克;压力容器;推进剂罐;固体推进剂火箭发动机; spaCE sHUTTLE BOOsTERs; spaCE sHUTTLE ORBITERs;航天器配置;液氢;液体氧气; spaCE sHUTTLE paYLOaDs;

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专利

1. HIGH DENSITY LIQUID ROCKET BOOSTERS FOR THE SPACE SHUTTLE [J] . STEVEN S.PIETROBON Journal of the British Interplanetary Scoiety . 1999,第5a6期

机译：用于航天飞机的高密度液体火箭推进器
2. Cause-Consequence Analysis for NASA’s Space Transportation System (STS)-Solid Rocket Booster (SRB) [J] . Kouroush Jenab, Sam Khoury, Troy Fine, International Journal of Business and Management . 2015,第8期

机译：NASA太空运输系统（STS）-固体火箭助推器（SRB）的因果分析
3. Crane-load contact sensor: In the past, a laser alignment tool proved inaccurate in determining whether the Shuttle External Tank (ET) was floating, resulting in the ET swinging and hitting nearby structures causing damage to the flight element [J] . Nicholas Sheble InTech . 2005,第12期

机译：起重机载荷接触传感器：过去，激光对准工具被证明不能确定航天飞机外部储罐（ET）是否漂浮，从而导致ET摆动并撞击附近的结构，从而损坏飞行元件
4. Computational Reentry Aerothermodynamics in the Aft Skirt Cavity Region of the Space Shuttle Solid Rocket Boosters [C] . C.C.Wu, R.W.Lycans, T.D.Haykin, 6th AIAA/ASME Joint Thermophysics and Heat Transfer Conference June 20-23, 1994/Colorado Springs, CO . -1

机译：航天飞机固体火箭助推器后裙腔区域的计算折返空气热力学
5. A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster. [D] . Cassibry, Phillip J. 2005

机译：太空运输系统固体火箭助推器上前后集成电子组件的可支撑性仿真。
6. The Secure Medical Research Workspace: An IT Infrastructure to Enable Secure Research on Clinical Data [O] . Michael Shoffner, Phillips Owen, Javed Mostafa, 2013

机译：安全的医学研究工作区：一种用于对临床数据进行安全研究的IT基础架构
7. Space Transportation System solid rocket booster thrust vector control system [O] . Potter J. H., Mccool A. A., Verble A. J. Jr. 1980

机译：航天运输系统固体火箭助推器推力矢量控制系统

Space Shuttle with rail system and aft thrust structure securing solid rocket boosters to external tank

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