1) reduced smoke propellant
少烟推进剂
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) smokeless NEPE propellant
微烟NEPE推进剂
1.
The effect of two copper compounds (AD and BC) and three carbon black on combustion characteristics of smokeless NEPE propellant are studied by determining the combustion characteristics of propellant at different pressures and analyzing the composition of elements on quick quenched surface.
通过测定不同压力下推进剂的燃烧性能及熄火表面元素分析,研究了两种铜盐(AD和BC)和3种碳黑对微烟NEPE推进剂燃烧性能的影响。
5) SP
无烟固体推进剂
6) pyrotechnic propellant
烟火型推进剂
补充资料：少烟推进剂
分子式：
CAS号：
性质：其燃气中没有（或只有少量）一次烟，允许有可接受的二次烟。少量一次烟主要指由燃速催化剂或燃烧稳定剂形成的烟。某些国家认为少烟推进剂是在6096m以上空域允许50%的时间形成终结尾流。该推进剂组分中不含铝粉（或只含少量铝粉），高氯酸铵少量。
CAS号：
性质：其燃气中没有（或只有少量）一次烟，允许有可接受的二次烟。少量一次烟主要指由燃速催化剂或燃烧稳定剂形成的烟。某些国家认为少烟推进剂是在6096m以上空域允许50%的时间形成终结尾流。该推进剂组分中不含铝粉（或只含少量铝粉），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