1.
Research on the catalytic thermal decomposition of RDX-CMDB propellants by TG-DSC-IR-MS
TG-DSC-IR-MS联用研究RDX-CMDB推进剂催化热分解
2.
Effects of DNP on Thermolysis and Combustion Characteristics of CMDB Propellant
DNP对CMDB推进剂燃烧性能及热分解的影响
3.
Effects of granularity of ammonium perchlorate on thermal decomposition of AP-CMDB propellant
高氯酸铵粒度对AP-CMDB推进剂热分解特性的影响
4.
gas propellents for aerosols
烟雾剂用气体推进剂
5.
NPP (Naval Propellant Plant)
海军火箭推进剂工厂
6.
slow surfactant slug
慢速推进活性剂段塞
7.
hybrid propellant rocket engine
混合推进剂火箭发动机
8.
propellant-based technology
推进剂燃烧压裂工艺
9.
PLCU (Propellant Level Control Unit)
推进剂水平控制设备
10.
Modeling of RDX/AMMO-BAMO pseudo-propellant combustion
RDX/AMMO-BAMO推进剂燃烧模型
11.
The nitroguanidine is added to the propellant during its mixing phase.
在推进剂的混合阶段将硝基胍加到推进剂中。
12.
Some propellant droplets may not evaporate within the confines of the thrust chamber.
有些推进剂可能在推力室内并未汽化。
13.
Study on the Processing Aids for Nitrate Plasticized Polyether Propellant
硝酸酯增塑聚醚推进剂工艺助剂研究
14.
Current Research Situation of Stabilizer for NEPE Propellants
NEPE推进剂用安定剂的研究现状
15.
Effect of potassium salt flame suppressors on the thermal decomposition behavior of the combustion catalysts used in solid propellant
钾盐消焰剂对推进剂催化剂热分解行为的影响
16.
Propellant Injection Vent rigs have been changed into Auxiliary Thrusters rigs.
推进剂填装管改装件已变更为辅助推进器。
17.
Study on the Software of Configuration Analysis of Liquid Propellant Space Propulsion Systems;
液体推进剂空间推进系统构型分析软件研究
18.
For proper combustion it is necessary to atomize the propellants.
为了有效地进行燃烧，推进剂必须雾化。