Evaluation of a Single-Stage Light-Gas Gun Facility in Malta: Business Analysis and Preliminary Design

L. Barilaro, L. Olivieri, R. Tiscio, A. Francesconi
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引用次数: 3

Abstract

Impact testing is a critical activity for many aerospace activities. Data on impacts can be employed to evaluate materials survivability, operations safety, and, if possible, to plan prompt maintenance. A classical impact testing facility usually employs Light-Gas Guns (LGGs) to evaluate the effect of collisions in a controlled laboratory environment. In particular, single stage LGGs are relatively simple in their working principle, as they consist in a pressurized gas reservoir and a barrel with a projectile placed in front of the experiment target. When the shot command is executed, the gas from the reservoir accelerates the projectile through the barrel; in first approximation, its velocity is related to the reservoir pressure, the barrel geometry, and the projectile velocity. In this context, The Malta College of Arts, Science and Technology (MCAST) and the Centre of Studies and Activities for Space CISAS “Giuseppe Colombo” of the University of Padova have started a collaboration to develop a single stage LGG impact facility in Malta. In this paper, the conceptual evaluation and the development of the facility is introduced. First, the potential application of such facility in the framework of Malta aviation market as well as the business opportunities in the emerging space sector are presented. In a second part of this work, the LGG main design drivers are defined and a preliminary evaluation of the achievable projectile velocities is performed.

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马耳他单级光气枪设施的评估:商业分析和初步设计
冲击试验是许多航空航天活动的一项关键活动。有关影响的数据可用于评估材料的生存能力、操作安全性,并在可能的情况下计划及时维护。经典的碰撞测试设施通常使用轻气枪(LGG)在受控的实验室环境中评估碰撞的影响。特别是,单级LGG的工作原理相对简单,因为它们由一个加压储气罐和一个在实验目标前放置有抛射物的枪管组成。当执行射击命令时,储气罐中的气体会加速炮弹穿过枪管;在第一近似中,其速度与储层压力、枪管几何形状和射弹速度有关。在这方面,马耳他艺术、科学和技术学院(MCAST)和帕多瓦大学空间CISAS“Giuseppe Colombo”研究与活动中心已开始合作,在马耳他开发一个单级LGG撞击设施。本文介绍了该设施的概念评价和发展情况。首先,介绍了这种设施在马耳他航空市场框架内的潜在应用以及新兴航天部门的商业机会。在这项工作的第二部分中,定义了LGG的主要设计驱动因素,并对可实现的射弹速度进行了初步评估。
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