摘要: Studies were made in support of production programs for Wing VI Minuteman second-stage motors. Summaries follow for the nine areas of program effort discussed. (1) Studies were made of various injectant-type TVC systems that could... 展开
作者 | Childres, H. E. | ||
---|---|---|---|
原报告号 | AD479205 | 总页数 | 200 |
主办者 | Non Paid Delimited ADS | ||
报告分类号 | [81G - Rocket Engines & Motors, 75 - Missile Technology] | ||
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Second-stage motors Surface to surface missiles Performance(Engineering) Secondary injection Thrust vector control systems Injection Solid propellant rocket engines Glass textiles Dacron Tape wound construction Loading Weight Thermal insulation Composite materials Roll Solid rocket propellants Rocket igniters Elastomers Stresses Thermal analysis O rings Test methods Optimization Ignition Rocket engine cases Joints Rocket nozzles Litvc(Liquid injection thrust vector control) Minuteman Nomex Submerged nozzles Viton fluoroelastomers |