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SPACECRAFT ROBUSTNESS TO ORBITAL DEBRIS

机译:航天器对轨道碎片的坚固性

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The ever increasing number of orbital debris has already ledrnthe space community to implement guidelines andrnrequirements for “cleaner” and “safer” space operations asrnnon-debris generating missions and end of mission disposal inrnorder to get preserved orbits rid of space junks. It is nowadaysrnwell-known that man-made orbital debris impacts are now arnhigher threat than natural micro-meteoroids and that recentrnevents intentionally or accidentally generated so many newrndebris that may initiate a cascade chain effect known as “thernKessler Syndrome” potentially jeopardizing the useful orbits.rnThe main recommendations on satellite design is torndemonstrate an acceptable Probability of Non-Penetrationrn(PNP) with regard to small population (<5cm) of MMODrn(Micro-Meteoroids and Orbital Debris). Compliance impliesrnto think about spacecraft robustness as redundancies,rnsegregations and shielding devices (as implemented in crewedrnmissions but in a more complex mass – cost – criticality tradeoff).rnConsequently the need is non-only to demonstrate thernPNP compliance requirement but also the PNF (probability ofrnNon-Failure) per impact location on all parts of the vehiclernand investigate the probabilities for the different fatalrnscenarios: loss of mission, loss of spacecraft (spacernenvironment critical) and spacecraft fragmentation (spacernenvironment catastrophic).rnThe recent THALES experience known on ESA Sentinel-3, ofrnincreasing need of robustness has led the ALTRAN companyrnto initiate an internal innovative working group on thoserntopics which conclusions may be attractive for their primernmanufacturer customers.rnThe intention of this paper is to present a status of this study :rn1.Regulations, requirements and tools availablern2.Detailed FMECA studies dedicated specifically tornthe MMOD risks with the introduction of new ofrnprobability and criticality classification scales.rn3.Examples of design risks assessment with regard tornthe specific MMOD impact risks.rn4.Lessons learnt on robustness survivability of systemsrn(materials, shieldings, rules) coming from otherrnindustrial domains (automotive, military vehicles)rn5.Guidelines and Recommendations implementablernon satellite systems and mechanical architecture.
机译:越来越多的轨道碎片已经促使航天界执行“更清洁”和“更安全”的太空操作的准则和要求,即无碎片产生飞行任务和任务结束处置的混乱,以使保留的轨道摆脱空间垃圾。如今,众所周知,人造轨道碎片撞击比自然的微流星体受到的威胁更大,而且最近的事件有意或无意中产生了如此多的新碎片,它们可能引发称为“瑟恩·凯斯勒综合症”的级联链效应,有可能危害有用的轨道。 rn关于卫星设计的主要建议是证明MMODrn(微流星体和轨道碎片)的人口少(<5cm)具有不渗透的概率(PNP)。合规性意味着必须将航天器的稳健性视为冗余,隔离和屏蔽设备(在机组人员任务中实施,但要在更复杂的质量-成本-临界度之间进行权衡)。因此,不仅需要证明PNP合规性要求,而且还需要证明PNF(概率为非-在各个部位的撞击位置发生故障),并调查不同致命情况的概率:任务损失,航天器损失(对航天环境至关重要)和航天器破碎(对航天环境造成灾难性破坏)。rn在ESA Sentinel-3上已知的最近THALES经验,日益增长的鲁棒性需求导致ALTRAN公司组建了一个针对这些主题的内部创新工作组,其结论可能对其底漆制造商客户具有吸引力。rn本文的目的是介绍本研究的现状:rn1,法规,要求和可用工具rn2。详细的FMECA研究专用规范通过引入新的概率和临界度分类表来拉扯MMOD风险。rn3。关于特定的MMOD冲击风险的设计风险评估示例。rn4。从其他工业领域获得的系统鲁棒性(材料,屏蔽,规则)的经验教训(汽车,军用车辆)rn5。实施准则和建议书的非卫星系统和机械结构。

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  • 来源
    《Safety is not an option》|2013年|1-10|共10页
  • 会议地点 Montreal(CA)
  • 作者单位

    ALTRAN Portugal, 2 rue des Cormorans, F-06210 Cannes, Email: stephane.heinrich@altran.com;

    ALTRAN France, 2 rue des Cormorans, F-06210 Cannes, Email: damien.legloire@altran.com;

    ALTRAN France, 2 rue des Cormorans, F-06210 Cannes, Email: andrea.tromba@altran.com;

    ALTRAN France, 1330 rue Guillibert de la Lauzière, F-13797 Aix , Email: michel.tholot@altran.com;

    ALTRAN France, 2 rue Paul Vaillant Couturier, F-92300 Levallois-Perret, Email: olivier.nold@altran.com;

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  • 正文语种 eng
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