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- The article studys the diffuser in the active injector altitude simulated test system of solid rocket engine. 对固体火箭发动机主动引射高空模拟试车系统中的扩压器部分进行研究。
- Flow field of unfold course for a solid rocket engine with extendible nozzle was analyzed by approach numerical solution of the 2-D axis symmetry N-S equation through AF method. 文中通过AF方法求解二维轴对称N-S方程,对采用延伸喷管+的固体火箭发动机级间展开过程地面单试的流场进行了数值分析。
- This thesis mainly described application situtition,application scope and testing technology feature for high energy ICT(Industrial Computed Tomography) in testing solid rocket engine. 本文主要介绍了大型高能工业CT在固体火箭发动机装药质量检测方面的应用现状、适用范围及工艺特点。
- The Analysis of Test Failure of Solid Rocket Engine 固体火箭发动机试验故障分析
- MODAL ANALYSIS OF SOLID ROCKET ENGINE SHELL 固体火箭发动机壳体的模态分析
- solid rocket engine specific impulse 固体发动机比冲
- The oscillatory combustion in solid rocket engines can be determined by comparing the pressure measured with copper post gauge to the maximum pressure measured with static electrical measurement system. 因此，用钢柱测压器测出的压强值与稳态压强电测系统测出的最大压强相比较，可以初步断定固体火箭发动机是否存在振荡燃烧现象。
- STUDY ON ZERO POINT VARIATION OF SOLID ROCKET ENGINE TESTING SYSTEM 固体火箭发动机试验测量系统零位变化研究
- ANALYSIS ON RELIABILITY GROWTH FOR A CERTAIN SOLID ROCKET ENGINE 某型固体火箭发动机的可靠性增长分析
- Analysis of Failure and Optimization for Composite Case of Solid Rocket Engine 固体火箭发动机复合材料壳体破坏分析及优化
- The Building of Coorperate Design Enviroment for PDM- based Solid Rocket Engine 基于PDM的固体火箭发动机协同设计环境研究
- Establishment of Mechanical Model of High-speed and High-acceleration Solid Rocket Engine Case 高速高加速固体火箭发动机壳体力学模型的建立
- An Assessment of the Flexing Stress of the Solid Rocket Engine Shell Under the Condition of the Complex Load 复杂受载条件下固体火箭发动机壳体屈曲应力的估计
- NUMERICAL SIMULATION OF INFRARED RADIATION PROPERTIES OF SOLID ROCKET ENGINE EXHAUST PLUME 固体火箭发动机尾喷焰红外特性数值模拟
- Kinematics Analyzed of a Virtual Axis Machine Tool Applied in Solid Rocket Engine Grain Machining 固体火箭发动机药柱整形虚拟轴机床的运动学分析
- INVESTIGATION ON OPENING AND THROWING OF AEROPLANE CANOPY BY USING SOLID ROCKET ENGINE 用固体火箭发动机抛放飞机座舱盖的探索
- Keywords SUBJECT TERMS Smoke abatement Combustion inhibitor Smolleless propellant Solid rocket engine; 消烟;燃烧抑制剂;无烟推进剂;固体火箭发动机;
- For one thing, they simplify the design of a rocket engine. 首先，它们可以简化火箭发动机的设计。
- The external tank and solid rocket boosters are waiting in the VAB. 航天飞机外贮箱和火箭推进器就在该中心等待装配。
- The rocket engine carries with it the oxygen of its own . 火箭发动机自带氧气。
