首页> 外文会议>Proceedings of the 7th European symposium on aerothermodynamics. >INTERMEDIATE EXPERIMENTAL VEHICLE, ESA PROGRAM IXV ATDB TOOL AND AEROTHERMODYNAMIC CHARACTERIZATION
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INTERMEDIATE EXPERIMENTAL VEHICLE, ESA PROGRAM IXV ATDB TOOL AND AEROTHERMODYNAMIC CHARACTERIZATION

机译:中级实验车辆,ESA计划IXV ATDB工具和气动热力学特性

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摘要

In the complex domain of the space technologies andrnamong the different applications available in Europe, arngreat interest has been placed since several years in therndevelopment of re-entry technologies. Among therndifferent achievements obtained in that field it is to bernrecalled the experience of the Atmospheric Re-entryrnVehicle flight in 1998 and a certain number ofrnimportant investments per-formed at Agency andrnnational levels like Hermes, MSTP, Festip, X-38,rnFLPP, TRP, GSTP, HSTS, AREV, Pre-X.rnIXV (Intermediate eXperimental Vehicle) builds onrnthese past experiences and studies and it is conceivedrnto be the next technological step forward with respectrnto ARDrnWith respect to previous European ballistic or quasiballisticrndemonstrators, IXV will have an increased inflightrnmanoeuvrability and the planned mission willrnallow verifying the performances of the requiredrntechnologies against a wider re-entry corridor. Thisrnwill imply from the pure technological aspect tornincrease the level of engagement on criticalrntechnologies and disciplines likernaerodynamics/aerothermodynamics, guidance,rnnavigation, control, thermal protection materials and inrnflight measurements.rnIn order to support the TPS design and the other subsystems,an AeroThermodynamicDataBase Tool hasrnbeen developed by Dassault Aviation and integrated byrnThales Alenia Space with the Functional EngineeringrnSimulator (used for GNC performances evaluation) inrnorder to characterize the aerothermodynamic behaviourrnof the vehicle.This paper will describe:1. The methodology used to develop the ATDB tool,based on the processing of CFD computations andWTT campaigns results.2. The utilization of the ATDB tool, by means of its integration into the System process. 3.The methodology used for the aerothermal characterization of IXV.
机译:在空间技术的复杂领域和在欧洲可用的各种应用中,自几年以来,人们一直对重新进入技术的发展抱有极大的兴趣。在该领域获得的不同成就中,有一种被称为1998年“大气再进入”飞行的经历,以及在原子能机构和国家一级进行的一些重要投资,例如爱马仕(Hermes),MSTP,Festip,X-38,rnFLPP,TRP, GSTP,HSTS,AREV,Pre-X.rnIXV(中级实验车辆)建立在过去的经验和研究基础之上,并且被认为是ARDrn的下一步技术进步。相对于先前的欧洲弹道或准弹道式示威者,IXV的飞行机动性和可操作性将增强计划中的任务将允许在更宽的重入通道上验证所需技术的性能。这将意味着从纯粹的技术角度出发,提高对空气动力学/空气动力学,指导,导航,控制,热保护材料和飞行测量等关键技术和学科的参与程度。为了支持TPS设计和其他子系统,已经开发了AeroThermodynamicDataBase Tool由Dassault Aviation公司提供,并由Thales Alenia Space公司与功能工程仿真器(用于GNC性能评估)集成,以表征车辆的空气动力特性。本文将描述:1。基于CFD计算和WTT活动结果开发ATDB工具的方法2。通过将ATDB工具集成到系统过程中来进行利用。 3.用于IXV空气热表征的方法。

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    Thales Alenia Space Italia, Strada Antica di Collegno, 253 – 10146 Torino, Italy– Vincenzo.Mareschi@thalesaleniaspace.com;

    Thales Alenia Space Italia, Strada Antica di Collegno, 253 – 10146 Torino, Italy– Daniela.Ferrarella@external.thalesaleniaspace.com;

    Thales Alenia Space Italia, Strada Antica di Collegno, 253 – 10146 Torino, Italy– Elio.Zaccagnino@external.thalesaleniaspace.com;

    Dassault Aviation, 78, quai Marcel Dassault – Cedex 300 – 92552 Saint-Cloud Cedex , France–Jean-Pierre.Tribot@Dassault-Aviation.com;

    Dassault Aviation, 78, quai Marcel Dassault – Cedex 300 – 92552 Saint-Cloud Cedex , France, Jean-Jacques.Vallee@Dassault-Aviation.com;

    DEIMOS Space S.L.U., Ronda de Poniente, 19, 28760 Tres Cantos, Madrid, Spain.- Rodrigo.Haya@deimos-space.com;

    European Space Agency, 8-10 rue Mario-Nikis, 75738 Paris Cedex 15, France, - Giuseppe.Rufolo@esa.int;

    European Space Agency, 8-10 rue Mario-Nikis, 75738 Paris Cedex 15, France – Salvatore.Mancuso@esa.int;

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  • 正文语种 eng
  • 中图分类 航天(宇宙航行);
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