1.
Uniformity and Stability of Combustion Heat and Its Uncertainty Analyses for Mg/Al Fuel-rich Propellant
镁铝富燃料推进剂热值的均匀性和稳定性及不确定度分析
2.
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
3.
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
4.
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
5.
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
6.
The characterization of the combustion properties of the aluminum? magnesium fuel? rich propellant for unchoked ducted rocket was studied.
系统研究了铝镁贫氧推进剂低压燃烧特性的表征方法。
7.
Numerical simulation of deposition for aluminum/magnesium-loaded fuel-rich propellant ducted rockets
铝镁贫氧推进剂固冲发动机沉积数值模拟
8.
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
9.
Application Progress of Metal Fuels in Solid Propellants
金属燃料在固体推进剂中的应用进展
10.
A mass of solid propellant.
块状燃料一块固体推进剂
11.
Propellant is another term for the fuel of a rocket.
推进剂是火箭燃料的另一术语。
12.
The Technology of Aggregated Boron and Its Application in the Fuel-rich Solid Propellant;
硼团聚技术及其在富燃推进剂中的应用研究
13.
Thermal Analysis of Viton A/Mg/NaNO_3 Fuel Rich System
氟橡胶/镁/硝酸钠富燃料体系的热分析
14.
Effect of Magnesium Based Hydrogen Storage Materials on the Properties of Composite Solid Propellant
镁基储氢材料对AP/Al/HTPB复合固体推进剂性能的影响
15.
propellant-based technology
推进剂燃烧压裂工艺
16.
Modeling of RDX/AMMO-BAMO pseudo-propellant combustion
RDX/AMMO-BAMO推进剂燃烧模型
17.
Magnesium-Aluminium Layered Double Hydroxide by Liquid Coprecipitation Method and Its Flame Retardancy;
液相沉淀法制备镁铝水滑石阻燃剂及其阻燃性能的研究
18.
A rocket propellant consisting of a single substance or mixture that contains both fuel and oxidizer.
单元推进剂一种含有单一物质或燃料和氧化剂混合物的火箭推进剂