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Sub-Scale Orion Parachute Test Results from the National Full-Scale Aerodynamics Complex 80- By 120-ft Wind Tunnel

机译:国家规模的空气动力学综合大楼80-120英尺风洞的小规模猎户座降落伞测试结果

摘要

A two-week test campaign was conducted in the National Full-Scale Aerodynamics Complex 80 x 120-ft Wind Tunnel in support of Orion parachute pendulum mitigation activities. The test gathered static aerodynamic data using an instrumented, 3-tether system attached to the parachute vent in combination with an instrumented parachute riser. Dynamic data was also gathered by releasing the tether system and measuring canopy performance using photogrammetry. Several canopy configurations were tested and compared against the current Orion parachute design to understand changes in drag performance and aerodynamic stability. These configurations included canopies with varying levels and locations of geometric porosity as well as sails with increased levels of fullness. In total, 37 runs were completed for a total of 392 data points. Immediately after the end of the testing campaign a down-select decision was made based on preliminary data to support follow-on sub-scale air drop testing. A summary of a more rigorous analysis of the test data is also presented.
机译:为支持Orion降落伞摆活动,在国家全尺寸空气动力学综合大楼80 x 120英尺风洞中进行了为期两周的测试活动。该测试使用连接到降落伞通风口的仪器化3系绳系统以及仪器化降落伞立管,收集了静态空气动力学数据。还通过释放系绳系统并使用摄影测量法测量冠层性能来收集动态数据。测试了几种顶篷配置,并与当前的Orion降落伞设计进行了比较,以了解阻力性能和空气动力学稳定性的变化。这些配置包括具有不同水平和几何孔隙位置的顶篷,以及具有更高填充度的帆。总共完成了37次运行,共计392个数据点。测试活动结束后,立即根据初步数据做出了向下选择的决定,以支持后续的小规模空投测试。还介绍了对测试数据进行更严格分析的摘要。

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