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- Using parabolic trajectory of ballistic missile,surface to air missile with solid propellant can realize the aim of lesser weight and farther range. 地空導彈采用彈道導彈的拋物彈道技術(shù)，能夠實(shí)現應用固體推進(jìn)劑達到低質(zhì)量遠射程的目標。
- Abstract: Using parabolic trajectory of ballistic missile, surface to air missile with solid propellant can realize the aim of lesser weight and farther range. 文摘:地空導彈采用彈道導彈的拋物彈道技術(shù)，能夠實(shí)現應用固體推進(jìn)劑達到低質(zhì)量遠射程的目標。
- Using pintle technology, a conventional solid propellant rocket motor can provide variable thrust levels, increasing the energy utilizing efficiency and improving the capability of the missile. 喉栓式變推力發(fā)動(dòng)機可實(shí)現固體火箭發(fā)動(dòng)機的推力調節，提高能量利用效率，從多方面提升導彈武器的作戰效能，因此具有強烈的軍事需求。
- The fact proves that solid propellant could be possibly used as GDL fuel. 實(shí)驗結果表明，固體推進(jìn)劑可以 成為GDL燃料。
- The progress of the aging property of solid propellant were reviewed. 綜述了國內外推進(jìn)劑材料老化性能的研究進(jìn)展。
- Thus it can be concluded that the polygonal section missile body with a submerged inlet has a bright future in application. 可以推斷 ,多邊形截面彈體與埋入式進(jìn)氣道的組合具有光明的應用前景
- A mass of solid propellant. 塊狀燃料一塊固體推進(jìn)劑
- The visual-velocity increment and angle increment of missile body between samplings could be obtained by compensation algorithm. 通過(guò)補償計算,能夠得到彈體在采樣時(shí)間間隔內運動(dòng)的視速度增量和角增量。
- SPRINT (Solid Propellant Rocket Intercept Missile) 固體推進(jìn)火箭截擊導彈
- Bai Peng, Zhu Shoumei, Meng Yupeng, et al.The integrated computational simulation of the inner and outer flow field above the athodyd inlet/firebox and missile body [J]. 白鵬，朱守梅，孟宇鵬;等，沖壓發(fā)動(dòng)機進(jìn)氣道摻混段與彈體內外流場(chǎng)一體化數值模擬[J].;空氣動(dòng)力學(xué)學(xué)報;2005;23（1）：5-9
- Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems. 固體推進(jìn)劑發(fā)動(dòng)機系統的可調性基本上比液體或混合型的要差。
- The major scattering resource in top direction is radar antenna or infrared head, in side direction is dihedral reflector formed by missile wings, missile body and wings. 其主要散射源在頭向為雷達天線(xiàn)或紅外導引頭，在側向為彈翼之間的二面角以及彈身、彈翼。
- Solid Propellant Intercontinental Ballistic Missile 固體推進(jìn)劑洲際彈道導彈
- The output of strapdown seeker is not appropriate to be directly used in the control system of the missile,for it couples with the missile body angular motion. 捷聯(lián)導引頭輸出的信號中耦合有彈體姿態(tài)角運動(dòng)信號,不宜直接用于彈體控制。
- We shall try by means of a highly simplified development to expose certain advantages and disadvantages of solid propellant rocket systems. 我們想通過(guò)相當簡(jiǎn)單的推導來(lái)試圖闡明固體推進(jìn)劑火箭系統的某些優(yōu)缺點(diǎn)。
- So ADN is the first candidate oxidizer instead of AP in solid propellant in 21st century. 化學(xué)安定性和相容性滿(mǎn)足要求,故ADN將是21世紀首選的AP替代物。
- Herb Chelner,Jim Buswell,Dan evans.Embedded sensors for monitoring solid propellant grain. 余宏發(fā).;光纖傳感器在固體發(fā)動(dòng)機測試中的應用
- The pasty propellant is a new kind of chemical propellant derived from solid propellant. 膏體推進(jìn)劑是由固體推進(jìn)劑衍變而成的一種新型化學(xué)推進(jìn)劑。
- Solid Propellant Rocket Intercept Missile 固體推進(jìn)劑火箭攔截導彈
- J.J. Choury,carbon/carbon materials for nozzle of solid propellant rocket motors[J].AIAA76-609. 崔紅;李瑞珍;蘇君明等.;多元基體抗燒蝕炭/炭復合材料的微觀(guān)結構分析[J]
