1) negative-oxygen rich fuel propellant
负氧富燃料推进剂
2) Oxygen poor fuel rich propellant
贫氧富燃料推进剂
3) Oxygen-poor fuel-rich propellant
贫氧富燃料推进剂
4) fuel-rich propellant
富燃料推进剂
1.
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
2.
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
3.
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
5) fuel-rich solid propellant
富燃料推进剂
1.
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。
补充资料：七贫八富
1.见"七贫七富"。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条