Investigated charring erosive characters of internal insulation of solid rocket motor under flight acceleration.

研究了固体火箭发动机内绝热层在飞行加速度条件下的炭化烧蚀特性.

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Transformers do suffer from the internal short - circuit faults mainly due to internal insulation failure.

变压器内部短路故障发生的原因主要是变压器内部的绝缘失效.

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The experiment result can use to internal insulation design of solid rocket motor.

实验结果可作为发动机绝热层设计的依据.

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