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Zefiro 40 Solid Rocket Motor Technological and Programmatic Development Status

机译:Zefiro 40固体火箭发动机技术和程序开发状况

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In the frame of VEGA Evolution Program the development of a technological demonstrator, named Zefiro 40 Solid Rocket Motor, will allow to introduce the materials and technologies improvements able to increase the propulsive performance of VEGA Launcher solid rocket motors reaching a capability of greater payloads insertion in higher orbits. System analyses performed by ELV, Prime Contractor of VEGA Launcher, showed as possible step foreseeing the first stage propellant increase from 80 to about 145 tons and second stage propellant increase from 23 to about 40 tons. Zefiro 40 represents therefore the means for Avio S.p.A., leader in solid space propulsion and responsible of design and production of Zefiro 23 and Zefiro 9 SRMs, as well as P80 Loaded Motor Case, to develop innovative solutions with the primary target to increase the motor mass fraction, as an extremely low density thermal protection rubber, a high performance carbon-epoxy own pre-preg production, a self-protected nozzle flexible joint, an undercut casting design. The first insulated case development model realization at full scale is planned for the second half of the 2014. This paper reports the actual status of Z40 development: an overview of the performed activities is presented as well as the planned activities for the completion of the Zefiro 40 solid rocket motor development and qualification.
机译:在VEGA进化计划的框架内,开发名为Zefiro 40固体火箭发动机的技术演示器,将允许引入能够提高VEGA Launcher固体火箭发动机推进性能的材料和技术改进,从而实现更大的有效载荷插入能力更高的轨道。 VEGA Launcher的主要承包商ELV进行的系统分析表明,预见第一阶段推进剂将从80吨增加到约145吨,第二阶段推进剂从23吨增加到约40吨是可能的步骤。因此,Zefiro 40是固体推进器的领导者Avio SpA的手段,负责设计和生产Zefiro 23和Zefiro 9 SRM以及P80装载式电机外壳,以开发创新解决方案为主要目标,以增加电机质量分数,作为一种极低密度的热保护橡胶,一种高性能的碳环氧材料自己生产的预浸料,一种自我保护的喷嘴柔性接头,一种底切浇铸设计。计划在2014年下半年实现首个全面案例开发模型的实现。本文报告了Z40开发的实际状况:介绍了已开展的活动以及完成Zefiro的计划活动40固体火箭发动机的开发与鉴定。

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