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- Eagar M A,Jordan F W.A robust ballistic design approach for the space shuttle advanced solid rocket motor[R].AIAA 93-2058. 李曉斌;張為華;陳小前.;近似方法在多學科設計優化中的應用研究
- Four nozzles, canted outboard, split the exhaust of the solid rocket motor into four equal tails. 四個向外傾斜的噴管把固體火箭發動機的排氣流分成四個相等的尾巴。
- The influence of structure axial vibration on the internal ballistics of solid rocket motor was investigated. 文中研究了固體發動機結構的軸向振動對燃燒室內彈道性能的影響。
- Investigated charring erosive characters of internal insulation of solid rocket motor under flight acceleration. 研究了固體火箭發動機內絕熱層在飛行加速度條件下的炭化燒蝕特性。
- The thrust vector control(TVC) performance test of solid rocket motor is presented in this paper. 本文介紹了固體火箭發動機水下推力矢量特性試驗。
- A response surface method(RSM) for structure reliability analysis of solid rocket motor(SRM) grain was presented. 發展了一種固體火箭發動機葯柱結構可靠度分析的響應面法。
- Buckling analysis on rear dome of solid rocket motor case was studied by means of ANSYS. 用ANSYS軟體對固體發動機殼體后封頭進行了外壓屈曲分析。
- Crose J G.Reliability of solid rocket motor cases and nozzles[R].NTI S,N93-22103. 王松柏.;固體火箭發動機殼體結構的動態可靠性設計[J]
- Finite element method is used in the study of nozzle damping of instable combustion in a solid rocket motor. 應用有限單元法研究固體火箭發動機不穩定燃燒中的噴管阻尼，並用波衰減對比法進行了試驗研究。
- Carbon/carbon composites have become the most ideal materials for nozzles of solid rocket motor (SRM). 摘要C/C複合材料已成為固體火箭發動機(SRM)最理想的噴管材料。
- With the development of national defense and aerospace industry, detachmentdetection for solid rocket motor is the most pressing issue. 隨著國防和航空航天事業的發展,大型固體火箭發動機的脫粘檢測成為緊迫問題。
- The mechanism of solid rocket motor laser ignition,composition of practical laser ignition system and its key technologies are summaried. 概述了固體火箭發動機激光點火的機理、實用激光點火系統的組成和主要技術關鍵。
- The erosive property and principle of copper-infiltrated graphite as solid rocket motor(SRM) throat insert and tailpipe nozzle bushing are presented. 介紹了石墨滲銅材料作為固體火箭發動機(SRM)喉襯與長尾管襯套的燒蝕特性和機理。
- It is an effective new processing way for loading of the solid rocket motor with high loading density, high propellant mass fraction propellant. 為今後高裝填密度、高質量比的發動機裝葯開拓出一條新途徑。
- New insight also was offered on Chinese solid rocket motor technology work, important for both missile and space launch applications. 研究還提供了對於導彈和航天發射都具有重要影響的固體火箭發動機技術工作。
- The insulation layer, artificial debond layer and propellant grain in solid rocket motor chamber (SRM) are all polymer composite systems. 固體火箭發動機燃燒室內絕熱層、人工脫黏層及推進劑葯柱,均為高分子材料複合體系。
- The spinning solid rocket motor stability depends whether the small transverse angular velocity is exaggerated or diffused. 摘要旋轉固體火箭發動機是否穩定主要取決於其微小的側向角速度是否被耗散或被放大。
- China already has such segmented solid rocket motor and ramjet capabilities today, but scramjets are a much greater challenge. 中國已經擁有這種分離式火箭助推器和衝壓發動機技術，但超音速燃燒衝壓發動機是一個更大的挑戰。
- The filament-wound case (FWC) plays a more and more important role in the solid rocket motor chamber structure (SRMCS) with composite material widely used in spaceflight fields. 隨著複合材料在各個領域的廣泛應用，作為××××發動機燃燒室的纖維纏繞複合材料殼體在航天領域中越來越受到人們的重視。
- A kind of viscoelastic spectral stochastic finite element method(VSSFEM) was developed and stochastic analysis of solid rocket motor grains was presented. 發展了一種粘彈性譜隨機有限元法(VSSFEM),並將其用於固體火箭發動機裝葯結構隨機分析。
