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1)  low vulnerability
低易损性
1.
The experimental results indicate that the low vulnerability of rocket motor with steel case is low;the fragmentation of the propellant depend on the mechanical performance;and the combustion inten- sity is effected by the thickness along impactiv.
为了解HTPB和NEPE固体火箭发动机的冲击安全性,设计了模拟实验发动机,对不同的壳体材料、推进剂和沿受冲击方向的厚度开展了枪击低易损性试验研究。
2.
The main properties and low vulnerability tests of 40NTO/60TNT and 25RDX/25NTO/50TNT formulations are researched.
研究了两种含NTO的炸药配方 40NTO/ 60TNT和 2 5RDX/ 2 5NTO/ 5 0TNT的主要性能及低易损性
2)  LOVA
低易损性
1.
Study on LOVA Performances Test of a New Propelling Charge;
一种新型发射装药低易损性能的测试研究
3)  LOVA propellant
低易损性发射药
1.
The combustion properties of LOVA propellant were studied through closed vessel.
采用密闭爆发器试验手段,对低易损性发射药的燃烧性能进行了研究。
2.
The ignition and combustion experiments of two types of LOVA (Low Vulnerable Ammunition) propellants with the simulation equipment and the closed bomb showed that the ignition of the LOVA propellants with the common igniting agents is very difficult.
模拟装置和密闭爆发器 2种不同发射药点火燃烧试验表明 ,常规点火剂很难解决低易损性发射药 (LOVA发射药 )的点火问题 ,选择点火剂时应考虑点火剂的综合点燃能力 。
3.
By choosing the binds, plasticizers and burning modifiers, designing the formula and numerical calculating, the formulation of LOVA propellant has determined by using RDX as the main energetic composition with inert and energetic complex bi nders, complex plasticizers and combustion modifiers.
通过对低易损性发射药用粘结剂、增塑剂、燃烧改良剂的选择和配方设计及理论计算 ,并结合试验研究 ,对所设计配方的能量、燃烧及力学性能进行了试验论证 ,基本确定了以 RDX为含能填料、惰性和含能复合粘结剂、复合增塑剂及燃烧改良剂和力学性能改善剂所组成的低易损性发射药配方类型 ;证明了采用溶剂法挤压成型工艺技术路线的可行
4)  LOVA propellants
低易损性火药
5)  low vulnerability propellant
低易损性推进剂
6)  LOVE [英][lʌv]  [美][lʌv]
低易损性炸药
补充资料:低易损性推进剂
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性质:指对冲击、枪击和热感等外部激能作用敏感性小、不易发生燃烧转爆轰的推进剂。一般中能复合固体推进剂如丁羧、丁腈羧,丁羟固体推进剂均符合低易损性推进剂要求。机载、舰载战术武器,要求使用低易损性推进剂。

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