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finding---Delphi
- 固体火箭推进剂燃速查询系统源程序Delphi编写，非常小的程序，初学delphi的可以看看，有一定水平的就免了-solid rocket propellant burning rate Inquiry System source Delphi, very small procedures, delphi the novice can see a certain level of tax on the
hjtk
- 火箭腾空，适用于课程设计，C界面会出现火箭腾空的画面。-Rockets vacated apply to the curriculum design, C interface will be vacated rocket screen.
rockettheory
- 国外火箭理论论文，不错的资料 -Rocket theory papers overseas, good information, good information
rebdo-2.0.tar
- Utility to work with Rocket Eboo and REB-Utility to work with Rocket Eboo and REB1100
huojian
- 火箭发射程序，visual c++语言编写，用于模仿火箭发射的过程，设计简单，易于理解-Rocket program, visual c++ language, used to mimic the process of launching the rocket, designed to be simple, easy to understand
dandao2
- 大气中的火箭弹道模拟，考虑空气阻力因素，用4阶龙格库塔解运动方程-Atmospheric rocket trajectory simulation, considering air resistance factor, with fourth-order Runge-Kutta solution of the equations of motion
GUIDANCE
- 包括火箭主动段的标准轨道发射器以及主动段的显示制导制导律仿真-Guidance Guidance Law including the display emulation standard orbit rocket launchers active segment and active segment
rocket1
- 用visual basic编写的火箭弹膛内运动可视化界面及计算程序，模型简单，易使用-Written with the visual basic visual interface rocket the chamber movement and calculation procedures, the model is simple, easy to use
han1
- 这里我们针对三级固体火箭进行研究，主要考虑每一级发动机工作时推力 和比冲 与发动机试车存在摄动偏差（相差 ）时所产生火箭关机点时刻的状态偏差。火箭的飞行的动力学方程可建立在地面发射坐标系中，火箭的第一级、第二级和第三级按照固定的俯仰角程序飞行，第二、三级飞行时已在大气层外，此时可忽略气动力的影响。-Here we study for three solid rocket, the main consideration at every level when the engine thrust a
Rocket Science for Traders (John F. Ehlers)
- New interesting innovative trading indicators.
RD
- 该款软件用于火箭发动机性能参数计算，比如固体火箭发动机、液体火箭发动机等(This software is used for the performance calculation of rocket engine)