Thermally induced vibrations in inflatable space structures: theory and experiment

充气空间结构中的热致振动：理论与实验

• 批准号: 371472-2009
• 负责人: Salehian, Armaghan
• 金额: $ 2.04万
• 依托单位: University of Waterloo
• 依托单位国家: 加拿大
• 项目类别: Discovery Grants Program - Individual
• 财政年份: 2014
• 资助国家: 加拿大
• 起止时间: 2014-01-01 至 2015-12-31
• 项目状态: 已结题
• 来源: https://www.nserc-crsng.gc.ca/ase-oro/Details-Detailles_eng.asp?id=550051
• 关键词: Thermally; induced; vibrations; inflatable; space

One of the main obstacles to placing spacecrafts in orbits is their high price for launch. Therefore, weight has always been a major design concern for space industry. Inflatable technology is a promising solution for placing large metrology systems in space to meet their launch volume and mass goals. This emerging technology offers lightweight, stowable and deployable satellite systems that can be compressed into folded stacks of a few inches thickness during launch and can be inflated and deployed over hundreds of feet in space. Because these structures are stowed during launch and deployed only upon reaching the destination orbit, the critical loads and disturbances in space are of particular importance. This is in contrast with older satellites for which most critical loads are met during launch. One of the most important sources of environmental disturbance is the rapid temperature change encountered on passing through the Earth's shadow. Such disturbances can induce bending moments and torques in the structure which result in thermal oscillations that can corrupt the pointing accuracy and precision of the satellite system and can last anytime from a few hours to a year. Therefore, a major objective of the proposed research is to develop novel analytical and experimental techniques for investigation and characterization of thermal loads on some of the major components of inflatable structures such as rigidized booms and Mylar membranes. This study will investigate the dynamic response of these materials to rapid temperature changes. The experimental techniques along with complementary modeling methods for inflatable structures represent novel aspects of this work and will make a significant contribution to our understanding of the thermal dynamic behaviour of the inflatable structures. The results will be used to develop control techniques to minimize the susceptibility of such systems to thermal disturbances. The proposed research program is intended to train the next generation HQP in structural vibration and control, with experimental applications which are in demand by industrial companies such as COM DEV International Ltd., MDA and the Canadian Space program.

将航天器送入轨道的主要障碍之一是高昂的发射费用。因此，重量一直是航天工业的主要设计问题。充气技术是在太空放置大型计量系统以满足其发射体积和质量目标的一种有前途的解决方案。这项新兴技术提供了重量轻，可收起和可部署的卫星系统，可以在发射过程中压缩成几英寸厚的折叠堆栈，并可以在数百英尺的太空中充气和部署。由于这些结构在发射期间被收起，只有在到达目的地轨道时才展开，因此空间中的临界载荷和扰动特别重要。这与较老的卫星形成对比，后者在发射期间满足最关键的载荷。环境扰动的最重要来源之一是在穿过地球阴影时遇到的快速温度变化。这种扰动可能在结构中引起弯矩和扭矩，从而导致热振荡，这可能破坏卫星系统的指向准确度和精度，并且可能持续几个小时到一年的任何时间。因此，拟议的研究的一个主要目标是开发新的分析和实验技术的调查和表征的热负荷的一些主要组成部分的充气结构，如刚化的繁荣和聚酯薄膜。本研究将研究这些材料对快速温度变化的动态响应。实验技术沿着与补充建模方法的充气结构代表了这项工作的新方面，并将作出重大贡献，我们的理解的热动力学行为的充气结构。研究结果将用于开发控制技术，以尽量减少这种系统对热扰动的敏感性。拟议的研究计划旨在培养下一代结构振动和控制方面的HQP，并提供COM DEV International Ltd.等工业公司所需的实验应用，MDA和加拿大太空计划。