| 引用本文: | 王秉渊,戚正风.气象火箭隔热涂层的设计.[J].国防科技大学学报,1982,(2):79-94.[点击复制] |
| Wang Bingyuan,Qi Zhengfeng.Design of Heat-insulating Coating for the Meteorological Rocket[J].Journal of National University of Defense Technology,1982,(2):79-94[点击复制] |
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| 气象火箭隔热涂层的设计 |
| 王秉渊, 戚正风 |
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| 摘要: |
| 本文论及气象火箭头部锥壳的隔热涂层。在考虑了火箭头锥工作环境需要和可能的基础上，完成了材料在飞行环境下温度载荷的计算、涂层组成以及成型方法的选择。通过地面模拟实验确定了涂层的最佳厚度。最后通过飞行试验，证实了隔热涂层可供实际使用。 |
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| 投稿日期：1981-10-19 |
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| Design of Heat-insulating Coating for the Meteorological Rocket |
| Wang Bingyuan, Qi Zhengfeng |
| Abstract: |
| This paper deals with a cone heat-insulating coating of the meteorological rocket. On the basis. of the consideration for the environment conditions necessary and possible for the rocket cone，the following articles have been completed: Calculation of the temperature load for the materials in flight environments，selection of material of which the coating is composed and methods of shaping. The optimum thickness of the coating is determined by the simnlation experiments on the ground. Finally，the practical applicability of the heat-insulating coating is proved through the flight test. |
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