1) 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。
2) SP
无烟固体推进剂
3) smokeless modified double-base propellant
无烟改性双基推进剂
1.
The theoretical calculation results of energy characteristics for smokeless modified double-base propellant with ACP show that ACP can decrease the energy of the propellant.
含ACP的无烟改性双基推进剂能量特性理论计算表明,ACP对推进剂的能量影响较小。
2.
Four mathematical models describing the combustion of smokeless modified double-base propellant, which contain fast burning energetic substance with different shapes (cube,globular,cuboid,and slice), are established.
建立了含4种不同晶形快燃物(立方体、球形、长方体、片状)无烟改性双基推进剂的燃烧数学模型,推导出推进剂燃速数学表达式,以及在推进剂燃烧方向上快燃物有效使用粒径的数学表达式。
4) 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。
5) reduced smoke propellant
少烟推进剂
补充资料：无烟推进剂
分子式：
CAS号：
性质：其燃气中既没有(或只有少量)一次烟，又没有二次烟或入射波束沿排气羽焰X轴向直接穿过或倾斜7°角给出90％以上透明度的推进剂。该推进剂组分中不含铝粉和高氯酸铵，采用硝胺为氧化剂。有利于提高导弹武器的生存能力、命中精度和战斗力。
CAS号：
性质：其燃气中既没有(或只有少量)一次烟，又没有二次烟或入射波束沿排气羽焰X轴向直接穿过或倾斜7°角给出90％以上透明度的推进剂。该推进剂组分中不含铝粉和高氯酸铵，采用硝胺为氧化剂。有利于提高导弹武器的生存能力、命中精度和战斗力。
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