Effect of agglomerated boron on combustion properties of fuel-rich propellants;
团聚硼对富燃料推进剂燃烧性能的影响
Effect of oxidizer and agglomerated boron particle size on burning rate of fuel-rich propellants;
氧化剂和团聚硼粒度对富燃料推进剂燃速特性的影响
Energy properties and characteristic signal of fuel-rich propellants containing 3,4-diamino-furazan;
含3,4-二氨基呋咱低特征信号富燃料推进剂能量性能及特征信号分析
By these methods,the critical technologies,such as flow adaptability,deposition prevention for nozzle,fuel-rich solid propellant,and so on were developed,and many test data were got in this study.
非壅塞燃气发生器作为整体式固体火箭冲压发动机主级工作的核心部件,在研究过程中,以理论分析为基础,通过大量缩比发动机试验,突破了燃气流量自适应性技术、富燃料推进剂配方研究及喷管防沉积等关键技术,取得了大量试验数据和宝贵经验。
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
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
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
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
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
Application Progress of Metal Fuels in Solid Propellants
金属燃料在固体推进剂中的应用进展
A mass of solid propellant.
块状燃料一块固体推进剂
Propellant is another term for the fuel of a rocket.
推进剂是火箭燃料的另一术语。
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
propellant-based technology
推进剂燃烧压裂工艺
Modeling of RDX/AMMO-BAMO pseudo-propellant combustion
RDX/AMMO-BAMO推进剂燃烧模型
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
fuel cell electric propulsion apparatus
燃料电池电力推进装置
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
Liquid oxygen is used as an oxidant for liquid fuels in the propellant systems of missiles and rockets.
在导弹和火箭的推进系统中氧用作液体燃料的氧化剂。
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。
This giant booster probably burned the usual kerosene fuel and liquid-oxygen oxidizer rather than some new superfuel.
这巨大的推进器很可能燃烧普通煤油及液体氧气化剂而不是某种新超级燃料。
Modeling Missile Propellant Fires In Shipboard Compartments; Oct 98-Sep 99
军舰舱内导弹推进剂燃烧建模