首页> 外文会议>52nd International Astronautical Congress Oct 1-5, 2001 Toulouse, France >Strategies to launch Satellites with Electric Propulsion Systems on Ariane 5
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Strategies to launch Satellites with Electric Propulsion Systems on Ariane 5

机译:在阿丽亚娜5号发射带有电力推进系统的卫星的战略

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Geostationary communication satellites are classically delivered into the elliptical Geostationary Transfer Orbit (GTO). A large portion of the satellite's propellant is used for the transfer manoeuvre to Geostationary Orbit (GEO) and the satellite bus design is largely driven by the accommodation of propellant. Currently new satellite propulsion systems are under study, which potentially allow a more advanced bus design. The most radical solutions are satellites using electric propulsion systems not only for the orbital life phase, but also for a part of the transfer to GEO. These propulsion systems have specific impulses, characterising the system's efficiency, far beyond chemical systems and thus save mass. The problem is the low thrust level of such systems, which extends the transfer time to GEO and requires optimisation of the insertion orbits to be provided by the launcher. For the launch of such satellites, different initial orbits were studied by Astrium. Strategies comprise the launch into Medium Height Earth Orbits (MEO), Super GTO and GTO PLUS. To most of the new insertion orbits ballistic phases and upper stage re-ignition become mandatory. As there will be at least a long transition phase from chemical to electric satellites a mixed dual-launch into with a chemical and an electric satellite on a second orbit may occur, requiring an optimised injection strategy for the launcher. Besides the use of a re-ignitable upper stage, concepts with a dedicated transfer stage, were studied. The objective of the study carried out at Astrium was to assess the interest of electric propulsion for GEO satellites and the impacts on satellite and launcher. A further objective was to analyse whether Ariane 5 is well adapted to the launch of full electric satellites. Astrium Space Infrastructure builds the EPS (Storable Propellant Stage) upper stage, the AESTUS engine, the Vehicle Equipment Bay (VEB) and develops the ESC-A (Cryogenic Upper Stage) of Ariane 5. Furthermore Astrium provides thrust chambers and equipment for other Ariane 5 stages. Ariane 5 is a programme of the European Space Agency ESA. ESA has delegated the programme management to the French National Space Agency CNES.
机译:对地静止通信卫星通常被送入椭圆形对地静止转移轨道(GTO)。卫星推进剂的很大一部分用于对地静止轨道(GEO)的转移机动,而卫星总线的设计在很大程度上取决于推进剂的容纳范围。当前正在研究新的卫星推进系统,这可能允许更高级的总线设计。最根本的解决方案是使用电子推进系统的卫星,不仅用于轨道生命周期,而且用于向GEO转移的一部分。这些推进系统具有特定的推动力,其特征是系统的效率,远远超过化学系统,从而节省了质量。问题在于这种系统的推力水平低,这延长了向GEO的转移时间,并需要优化发射器要提供的插入轨道。为了发射此类卫星,Astrium研究了不同的初始轨道。策略包括发射到中高度地球轨道(MEO),超级GTO和GTO PLUS。对于大多数新的插入轨道来说,弹道阶段和上层重新点火是强制性的。由于从化学卫星到电卫星至少会有一个漫长的过渡阶段,因此可能会在第二轨道上发生化学物质和电卫星的混合双重发射,这需要发射器的优化注入策略。除了使用可重燃的上级之外,还研究了带有专用转移级的概念。在Astrium进行的研究的目的是评估对GEO卫星电力推进的兴趣以及对卫星和发射器的影响。另一个目标是分析阿丽亚娜5号是否完全适合发射全电卫星。 Astrium太空基础设施建造EPS(可存储推进剂阶段)上层,AESTUS发动机,车辆设备湾(VEB),并开发Ariane 5的ESC-A(低温上层)。此外,Astrium还为其他Ariane提供推力室和设备。 5个阶段。阿丽亚娜5号是欧洲航天局(ESA)的一项计划。 ESA已将程序管理权委派给法国国家航天局CNES。

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