The lighter version used liquid hydrogen, the heavier used hypergolic propellants.
较轻的推进器采用液态氢，较重的采用自燃推进剂。
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
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
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
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。
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
Modeling Missile Propellant Fires In Shipboard Compartments; Oct 98-Sep 99
军舰舱内导弹推进剂燃烧建模
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。
Propellant is another term for the fuel of a rocket.
推进剂是火箭燃料的另一术语。
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
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
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
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
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
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