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SNC Qwksep - A Simple, Reliable, Stiff and Low-Shock Separation System for Small Sat Missions

机译:SNC QWKSEP - 用于小型SAT任务的简单,可靠,坚硬和低震动的分离系统

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The SNC Qwksep technology is a Marman band retention system with a low shock release mechanism. The Qwksep is unique in that it combines flight heritage geometry and a Clamp Band Opening Device (CBOD), packages these features in a very small height envelope of 2 inches, and provides bolt circle interfaces for the launch vehicle and payload. The system developed targeted a specific set of requirements related to small satellites in the 600 to 1,100 pound size to demonstrate the technology as opposed to a specific product. An engineering unit was designed and built to demonstrate functionality and load capacity. Finite element analysis (FEA) was used in the design stage to predict stiffness and service load capability. The engineering unit was tested for function, stiffness, and load capacity. Test results were compared to analysis predictions and show very good correlation. The engineering unit was tested to an equivalent tensile load (P_(eq)) of 25,000 pounds. This load envelopes the target payload launch environment. Stiffness was measured at over 3.7 x 10~6 pounds per inch in axial tension. Correlated analysis predicts a tensile load capacity of 33,600 pounds for a 5,000-pound nominal band tension. The engineering unit tests successfully demonstrated that the technology is a viable alternative to other systems and is ready to satisfy mission requirements in the small satellite market. Sierra Nevada Corporation (SNC) Space Systems plans to have a new 15-inch diameter version qualified by the end of 2013.
机译:SNC QWKSEP技术是一个具有低震动机制的Marman带保留系统。 Qwksep是独一无二的,因为它结合了飞行遗产几何和夹具带打开装置(CBOD),将这些特征包装在2英寸的非常小的高度外壳中,并为发射车辆和有效载荷提供螺栓圈界面。该系统开发了与600至1,100磅尺寸的小卫星相关的特定要求,以证明该技术与特定产品相反。设计并构建了工程单元,以证明功能和负载能力。在设计阶段使用有限元分析(FEA)以预测刚度和服务负载能力。测试工程单元的功能,刚度和负载能力。将测试结果与分析预测进行比较,表现出非常好的相关性。将工程单元测试为25,000磅的等效拉伸载荷(P_(等式))。此负载封闭目标有效载荷发射环境。在轴向张力下以超过3.7×10〜6磅的3.7×10〜6磅测量刚度。相关性分析预测拉伸载荷容量为33,600磅,用于5,000磅的标称带张力。工程单元测试成功证明了该技术是其他系统的可行替代品,并准备好满足小型卫星市场的特派团要求。 Sierra Nevada Corporation(SNC)空间系统计划在2013年底拥有新的15英寸直径型。

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