1.
Modeling Missile Propellant Fires In Shipboard Compartments; Oct 98-Sep 99
军舰舱内导弹推进剂燃烧建模
2.
SPIRBM (Solid Propellant Intermediate Range Ballistic Missile)
固体推进剂中程弹道导弹
3.
A self-propelled missile, such as a rocket.
自动推进武器自动推进的导弹，比如火箭
4.
The Scale Effect of Cavitating Flow on the Jet-Propelled Missile
喷气推进导弹空泡流的尺度效应研究
5.
Using parabolic trajectory of ballistic missile, surface to air missile with solid propellant can realize the aim of lesser weight and farther range.
地空导弹采用弹道导弹的抛物弹道技术，能够实现应用固体推进剂达到低质量远射程的目标。
6.
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。
7.
Rockets are important as thrust units for ballistic missiles.
火箭作为弹道导弹的推力装置很重要。
8.
Simulation and Analysis for Attack-Defense Measures of Ballistic Missile during Boost Phase;
弹道导弹助推段攻防效能的仿真分析
9.
propellant gas producing cartridge
能产生推进气体的枪弹
10.
To attack with bombs, shells, or missiles.
炮击用炮弹、烟火弹或导弹进行攻击
11.
Abstract: Using parabolic trajectory of ballistic missile, surface to air missile with solid propellant can realize the aim of lesser weight and farther range.
文摘:地空导弹采用弹道导弹的抛物弹道技术，能够实现应用固体推进剂达到低质量远射程的目标。
12.
The formulae of optimal control overload commands are reckoned.
推导了基于捷联惯导控制方案的导弹最优控制过载指令公式,并进行了仿真验证。
13.
Study of Trajectory Optimization and Guidance Algorithm for Boost-Glide Missile
助推—滑翔导弹弹道优化与制导方法研究
14.
The Cox Report slanders China by saying it had "acquired" US missile guidance technology through commercial launches to promote the development of its own missiles.
《考克斯报告》诬称，中国通过商业发射“获缺了美国的制导技术并推进了中国导弹的发展。
15.
In the paper, the performance conjecture of TBM is discussed and the method to simulate TBM is presented.
讨论了战术弹道导弹性能推测及导弹仿真的实现方法。
16.
advanced medium-range air-to-air missile
先进中程空对东导弹
17.
Further more, how could the inference that such an improvement was "capable of being adapted for use as the guidance system for future PRC road-mobile intercontinental ballistic missiles'' be made?
进而这种改进“可能被中国用在未来公路机动发射型洲际导弹的系统上”的推论又如何得出？
18.
Modified Riemann-Liouville Fractional Order Derivative Definition in Solid Propellant Viscoelasticity Constitutive Model
一种改进的R-L分数阶导数定义在固体推进剂粘弹性本构模型中的应用