1.
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
2.
Iron oxide may be utilized in achieving propellants of ultrahigh burn rate.
氧化铁可用以制出超高燃速的推进剂。
3.
Study on the Formulation of Low Burning Rate HTPB Propellant with RDX
含RDX低燃速丁羟推进剂的配方研究
4.
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
5.
Correlation between Thermal Decomposition Characteristics and Burning Rate of GAP Fuel-Rich Propellants;
GAP贫氧推进剂热分解特性与燃速相关性研究
6.
Numerical Simulation for Burning Rate of Composite Modified Double Base Propellant Containing CL-20
含CL-20的改性双基推进剂燃速数值模拟
7.
Study on the Burning Rate Reference Materials for a Sort of Magnalium Low-oxygen Propellant
一种镁铝贫氧推进剂燃速标准物质研究
8.
propellant-based technology
推进剂燃烧压裂工艺
9.
Modeling of RDX/AMMO-BAMO pseudo-propellant combustion
RDX/AMMO-BAMO推进剂燃烧模型
10.
gas turbine booster propulsion set
增速燃气轮机推进装置
11.
gas turbine booster propulsion
燃气轮机加速推进装置
12.
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
13.
slow surfactant slug
慢速推进活性剂段塞
14.
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。
15.
Application Progress of Metal Fuels in Solid Propellants
金属燃料在固体推进剂中的应用进展
16.
A mass of solid propellant.
块状燃料一块固体推进剂
17.
Modeling Missile Propellant Fires In Shipboard Compartments; Oct 98-Sep 99
军舰舱内导弹推进剂燃烧建模
18.
Propellant is another term for the fuel of a rocket.
推进剂是火箭燃料的另一术语。