1532987 Solid fuel rocket motors DYNAMIT NOBEL AG 14 Nov 1975 [9 Dec 1974] 44752/75 Heading F3A A partition arrangement separating two coaxially aligned combustion chambers of a solid fuel rocket motor comprises, a cylindrical housing, means within the housing defining a single aperture co-axial...
Solid oxidizers provide oxygen needed to burn solid rocket motor fuel. By carrying fuel and oxidizer together, the rocket does not depend on the atmosphere for oxygen. Nitro-amines are not oxidizers per se; they are high explosives added to prop...
SOLID FUEL ROCKET MOTOR 专利名称：SOLID FUEL ROCKET MOTOR 发明人：AOKI ICHIROU 申请号：JP13711882 申请日：19820805 公开号：JPS5928055A 公开日：19840214 专利内容由知识产权出版社提供 摘要：PURPOSE:To stably fly at desired low speed by providing a partition wall between a propulsion nozzle and a ...
solid rocket 美 英 un.固体火箭;固体燃料火箭 网络固体液料火箭;固体火箭马达;用固体燃料推进的火箭 英汉 网络释义 un. 1. 固体火箭 2. 固体燃料火箭 释义: 全部,固体火箭,固体燃料火箭,固体液料火箭,固体火箭马达,用固体燃料推进的火箭
solid rocket [′säl·əd ′räk·ət] (aerospace engineering) A rocket that is propelled by a solid-propellant rocket engine. McGraw-Hill Dictionary of Scientific & Technical Terms, 6E, Copyright © 2003 by The McGraw-Hill Companies, Inc. ...
2) dry-fuel rocket,powder rocket,solid rocket,solid rocket unit 固体火箭<火> 3) solid rocket propellant 固体火箭推进剂 1. By studying and summing up the failure physical models in common use,this paper advanced a cumulative damage-reaction theory life model to the storage and usage of sol...
Numerically Enhanced Thermal Inspection of Shuttle Solid Rocket Motor Inhibitor/Liner/Fuel BondlineThe Solid Rocket Motors (SRM's) for the Space Shuttle are fabricated by laying up and molding materials, such as insulation, which are joined using adhesives, the adhesives being set along with the ...
By direct-conncted simulation calculation,the effects of common heater fuel (hydrogen,kerosene,methane and alcohol) on performance of solid ducted rocket motor with low-oxygen boron-based propellant were investigated. 通过直连模拟计算,研究了常用加热器燃料(氢气、煤油、甲烷和酒精等)对含硼贫氧推进剂...
The pulse detonation rocket engine(PDRE)with variable cross-section was investigated using kerosene as fuel and oxygen as oxidizer at the equivalence ratio 1. 0的条件下,进行了变截面脉冲爆震火箭发动机的实验研究,其中包括等截面发动机,扩张型发动机,收敛型发动机,扩张-收敛型以及收敛-扩张型发动机。 更多...
1.In order to judge the stability of the surface crack insolid rocketmotor (SRM) grains while the SRM was launched in different environmental temperature.为了探讨环境温度对固体火箭发动机点火发射时药柱内表面裂纹稳定性的影响,以翼锥-过渡伞盘-圆柱组合药型的发动机为例,采用三维有限元方法,在发动机药柱...