1.
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
2.
Improvement of processing property of high energy fuel-rich HTPB propellant containing boron
高能含硼贫氧推进剂工艺性能改善研究
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.
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
5.
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。
6.
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。
7.
Study on Hydrazine Wastewater Treatment by Catalytic Oxidation;
肼类推进剂废水的催化氧化处理研究
8.
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
9.
In using Eq. 3-1 of course one first identifies the fuel molecules and the oxidizer molecules of the propellant.
当然，应用式（3-1）时首先要辨明推进剂的燃烧分子及氧化剂分子。
10.
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。
11.
"We should intensify our efforts to fight poverty through development, Build on the achievements we have scored in this regard."
继续大力推进扶贫开发,巩固扶贫成果.
12.
Extending Improved Variety of Seed and Good Method to Eliminating Poverty and Get Rich in Poverty Hill Region;
推广良种良法促进贫困山区脱贫致富
13.
gas propellents for aerosols
烟雾剂用气体推进剂
14.
The most flux of the propellant depends on the self-pressurizing ability of the nitrous oxide supply system.
推进剂最大流量依赖于一氧化二氮供应系统自身增压能力。
15.
Investigation on Characteristics and Influencing Factors of Oxidation Process of UDMH
液体推进剂偏二甲肼氧化变质的规律和影响因素
16.
Cycle Power Balance Analysis for Liquid Rocket Engine with LO_2/RP-1 Propellant Combination
液氧/煤油推进剂液体火箭发动机循环动力平衡分析
17.
Study on EO-THF Copolymer Reference Materials Used in Solid Propellant;
高能固体推进剂用聚（环氧乙烷—四氢呋喃）标准物质的研究与制备
18.
Energy Characteristics Computation of Propellant Containing 3,3′-Dinitro-4,4′-oxazafurazan
含3,3′-二硝基-4,4′-氧化偶氮呋咱推进剂的能量特性研究