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Challenges of transferring the HEMP-Thruster based Ion Propulsion System from HispaSat to Heinrich Hertz

机译:将大麻拉丝的离子推进系统从Heinrich Hertz转移到Heinrich赫兹的挑战

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In 2008 German Aerospace Center - Space Administration (DLR) initially contracted Thales Deutschland GmbH to develop, construct, qualify and deliver a novel type of an ion propulsion system based on High Efficiency Multistage Plasma Thrusters (HEMP-T). The HEMP-T Assembly is being developed in the frame of the HEMP-TIS project (HEMP Thruster In orbit verification on SmallGEO) by the Business Unit Electron Devices of Thales Deutschland in Ulm. The HEMP-T Assembly consists of four HEMP-T Modules and one Power Supply and Control Unit PSCU which supplies the HEMP-T Modules with electric power and controls their operation. The HEMP-TIS project includes component development, system engineering, testing and qualification activities and the delivery of the respective flight units. Originally the Assembly was to fly on the Small Geostationary Satellite (SGEO) in ESA's ARTES 11 program. The platform was developed by OHB System for the HispaSat AG1 mission. Currently the change of the integration of the HEMP-T Assembly to the new Heinrich Hertz Mission is in preparation, which also uses the SGEO as platform. The transfer from HispaSat to Heinrich Hertz caused several challenges in the project lifecycle, especially in the fields of requirements engineering, qualification testing and components obsolescence management. The manufacturing and formal environmental qualification of all of the qualification units has been completed successfully. The units as well as the EQM power supply have successfully completed lifetime testing in June 2018 and therefore reached Technology Readiness Level (TRL) 8. The manufacturing of the flight units is completed and acceptance testing has been started. The respective PFM-PSCU has been delivered to Thales after successful acceptance testing, as well as the harness. All of these units have been subjected to End to End testing and confirmed the adequacy of the system design. The paper will give an updated status of the program and will focus on th
机译:2008年,德国航空航天中心 - 空间管理(DLR)最初收缩Thales Deutschland GmbH开发,构建,限定和提供基于高效多级等离子体推进器(HEMP-T)的小型离子推进系统。通过ULM的Thales Deutschland的商业单位电子设备,在HEMP-TIS项目(大麻推动器在SmallGeo上的轨道验证中的轨道验证中的大麻推进器的框架中开发了HEMP-T组件。 HEMP-T组件由四个HEMP-T模块和一个电源和控制单元PSCU组成,可提供电力的HEMP-T模块并控制其操作。 HEMP-TIS项目包括组件开发,系统工程,测试和资格活动以及交付各自的飞行单位。最初,大会是在欧安科艺术艺术品11节目中飞行小地静止卫星(SGEO)。该平台由OHB系统开发,用于Hispasat AG1 Mission。目前,HEMP-T组件整合到新的Heinrich Hertz任务的变化正在准备,这也使用SGEO作为平台。从Hyspasat转移到Heinrich Hertz在项目生命周期中引起了几个挑战,尤其是在需求工程,资格测试和组件过时管理领域。所有资格单位的制造和正式环境资格已成功完成。该单位以及EQM电源于2018年6月成功完成了终身测试,因此达到了技术准备水平(TRL)8.完成飞行单元的制造已完成,并已启动验收测试。在成功验收测试之后,相应的PFM-PSCU已被送到Thales,以及线束。所有这些单位都经过终端测试,并确认了系统设计的充分性。本文将提供该计划的更新状态,并将重点关注

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