1.
propellant-based technology
推进剂燃烧压裂工艺
2.
Modeling of RDX/AMMO-BAMO pseudo-propellant combustion
RDX/AMMO-BAMO推进剂燃烧模型
3.
Combustion Characteristics of Small Grain-Binding High-Burning-Rate Propellant;
小球粘结高燃速推进剂燃烧特性研究
4.
Modeling Missile Propellant Fires In Shipboard Compartments; Oct 98-Sep 99
军舰舱内导弹推进剂燃烧建模
5.
Electrical Conductivity of Combustion Products of Composite Propellant Containing Cs Salt
含Cs盐推进剂燃烧产物导电特性研究
6.
Influence of Fluorides on Combustion Characteristics of Mg/NaNO_3 Fuel-rich Propellants
氟化物对Mg/NaNO_3富燃料推进剂燃烧性能的影响
7.
Effect of coated and agglomerated boron on combustion characteristics of boron-based fuel-rich propellants
包覆及团聚硼对富燃料推进剂燃烧性能的影响
8.
Progress in combustion characteristic research of liquid rocket gelled propellants
液体火箭凝胶推进剂燃烧特性研究进展
9.
The Study of Combustion Characteristics of Solid Propellants under Laser Radiation
激光辐射下固体推进剂燃烧特性及规律研究
10.
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
11.
Application of Broadband CARS in Solid Propellant Combustion Field
宽带CARS在诊断固体推进剂燃烧场中的应用
12.
This deduction forms the basis of the two-temperature postulate for composite propellant combustion.
这种推理就是构成复合推进剂燃烧中两温概念的基
13.
Liquid propellant combustion processes are quite complicated and defy precise analytical description.
液体推进剂燃烧过程是相当复杂的，很难对其进行严谨的分析描述。
14.
Investigation on measuring gas generation rate for fuel-rich propellant during combustion process
富燃料推进剂的燃烧成气率测试研究
15.
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。
16.
Researches on Combustion and Processes of High Boron Content Boron-Based Fuel-Rich Solid Propellants;
高含硼富燃固体推进剂工艺和燃烧性能研究
17.
In using Eq. 3-1 of course one first identifies the fuel molecules and the oxidizer molecules of the propellant.
当然，应用式（3-1）时首先要辨明推进剂的燃烧分子及氧化剂分子。
18.
It will decrease the dark zone thickness and improve combustion performance by use of coeted boron with AP.
硼表面用AP包覆,可以降低暗区厚度,有利于改善推进剂的燃烧。