1) pyrotechnic propellant
烟火型推进剂
2) minimum smoke propellant
微烟推进剂
1.
Impact and Friction Sensitivity of Minimum Smoke Propellant Based on NC and TMETN;
以NC和TMETN为基的微烟推进剂机械感度研究
2.
In order to investigate the effect of novel energetic catalysts on the combustion properties of minimum smoke propellant, the RDX-CMDB propellant samples containing various energetic composite catalysts were prepared through a solventless extrusion technique.
为研究含能催化剂对微烟推进剂燃烧性能的影响,制备了多种含复合含能催化剂的RDX-CM DB推进剂,利用靶线法测定了推进剂在不同压力下的燃速,并对测试结果进行了线性回归。
3) smokeless propellant
无烟推进剂
1.
Replacing ammonium perchlorate with octanitrocubane in HTPB propellant increases the specific impulse for 125 N·s·kg-1,NC/NG/ONC smokeless MDB propellant has a specific impulse of 2545 N·s·kg-1,GAP/ONC/RDX smokeless propellant has a high specific impulse over 2600 N·s·kg-1 in very wide scope.
kg-1,由GAP/ONC/RDX组成的无烟推进剂,在很宽的范围内都可以得到2600N。
2.
GAP/TNAZ/RDX smokeless propellant has a high value of specific impulse over 2 600 N·s/kg in very wide scope.
s/kg;由GAP/TNAZ/RDX组成的无烟推进剂,在很宽的范围内都可得到2 600 N。
4) reduced smoke propellant
少烟推进剂
5) rocket propellant
火箭推进剂
1.
Hydroxylammonium nitrate(HAN) is a main component of the new liquid rocket propellants.
硝酸羟胺(hydroxylammon ium n itrate,HAN)是新一代液体火箭推进剂的主要成分,具有能量高、弹头初速高、易贮存和易操作等特点;但HAN可通过多种途径导致人体中毒,且中毒程度与其浓度及剂量呈正相关;可对人体肺脏、肝脏和血液等系统造成损伤。
2.
According to the complexity of precisely measuring propellant temperature before firing rocket projectiles, with present widely used computer numerical simulation method, the article has simulated 130 rocket propellant transient temperature field by program and also measured propellant temperature by designed experimental unit.
鉴于火箭弹发射前对推进剂温度精确测定的复杂性 ,利用目前应用广泛的计算机数值模拟技术 ,通过计算程序对 1 3 0火箭推进剂非稳态温度场进行了数值模拟 ,并利用设计的实验装置对推进剂的温度进行了试验测定 ,计算结果与测量点温度值吻合较好 ,得出了 1 3 0推进剂的非稳态温度场的变化规律及影响温度分布的主要热阻。
3.
Owing to peculiar function, working condition and safety requirement of rocket propellants, multiform protection means are necessary against them, especially preventing respiration organs of human body from hurting.
火箭推进剂由于其特殊作用、使用条件和安全要求,需采用多种防护手段对其防护,尤其是防止对人体呼吸器官的损伤。
6) Liquid rocket propellant
火箭推进剂
1.
This pap er summaries the application and development of respiratory protective equipment and analyses the protecting request against the liquid rocket propellant.
本文对呼吸防护装备的应用、发展进行了综述,分析了火箭推进剂毒性对呼吸防护的要求和国内推进剂呼吸防护研究现状,对推进剂专用呼吸防护装备的发展趋势进行了探讨。
补充资料：微烟推进剂
分子式：
CAS号：
性质：其燃气中没有(或只有少量)一次烟，允许有少量二次烟。少量一次烟主要指由燃速催化剂或燃烧稳定剂形成的烟。某些国家认为微烟推进剂是在8229m以下空域没有形成凝结尾流。该推进剂组分中不含铝粉，高氯酸铵少量。
CAS号：
性质：其燃气中没有(或只有少量)一次烟，允许有少量二次烟。少量一次烟主要指由燃速催化剂或燃烧稳定剂形成的烟。某些国家认为微烟推进剂是在8229m以下空域没有形成凝结尾流。该推进剂组分中不含铝粉，高氯酸铵少量。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条