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Analysis and test for thermal performance of High Altitude Super Pressure Balloons during ascending process

机译:高空超压气球上升过程中的热性能分析与测试

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A two-node model for thermal characteristics and a dynamic model of High Altitude Super Pressure Balloon (HASPB) during ascending process are established. The thermal performance of HASPB during ascending process is analyzed. Several simulations are conducted under the same conditions with the real flight test. Results show that supercool phenomenon occurs during ascending caused by free expansion of gas, and the value is about 10-15 K. Once the balloon reaches the design height and becomes over-pressured, the temperature of balloon rises rapidly, and this adjustment process lasts for about 10 minutes. The real flight test to 20000 m validates the reliability of the two-node model.
机译:建立了两节点热力特性模型和高空超高压气球上升过程的动力学模型。分析了HASPB在上升过程中的热性能。在真实的飞行测试中,在相同条件下进行了几次模拟。结果表明,气体自由膨胀引起的上升过程中出现过冷现象,其值约为10-15K。一旦气球达到设计高度并过压,气球温度迅速升高,这种调节过程持续进行大约10分钟。到20000 m的实际飞行测试验证了两节点模型的可靠性。

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