Novel Orbital Debris Protection of Spacecraft

新型航天器轨道碎片保护

基本信息

  • 批准号:
    RGPIN-2018-06050
  • 负责人:
  • 金额:
    $ 2.33万
  • 依托单位:
  • 依托单位国家:
    加拿大
  • 项目类别:
    Discovery Grants Program - Individual
  • 财政年份:
    2018
  • 资助国家:
    加拿大
  • 起止时间:
    2018-01-01 至 2019-12-31
  • 项目状态:
    已结题

项目摘要

Orbital debris poses a significant threat to space flight safety - even small particles can damage, degrade, or destroy spacecraft due to the very high velocities involved in a collision, which average about 9 km/s. The purpose of the proposed research program is to pursue research efforts in the field of Micrometeoroid and Orbital Debris (MMOD). ***There has been a dramatic rise in the density of orbital debris and this represents an ever-growing destructive threat to Canadian space assets. This is a strategic and economic concern for Canada due to the importance of these assets and the high cost associated with their manufacture and deployment. Due to the size of investments (such as $110 million dollar contract for the RADARSAT Constellation Mission program), Canadian Space Agency (CSA) has identified new defensive technologies as a key strategic priority for the Canadian space sector. Methods for debris impact modeling (which will include material, geometrical, and numerical models) need to be advanced in order to allow satellite vendors to investigate new shield configurations and predict their performance under impact stress. This will allow production of more durable space vehicles with longer lifespans that will ultimately prolong the functional duration of future Canadian space missions to the benefit of all Canadians.***The primary objective of this research program is to improve our understanding of MMOD impact processes. In so doing, it is expected to develop more accurate models of impact behavior which would be invaluable to satellite community to develop improved shielding and more durable satellite component designs. Considering the complex nature of hypervelocity impact phenomena and the variety of possible protection solutions, this work will require a combination of numerical and experimental study of hypervelocity impact on shield configurations to fully understand the physical processes and show the accuracy of the simulation models and methods used. The proposed program will address the protection of general spacecraft equipment, and will additionally focus on protection of composite overwrapped pressure vessels. When a pressure vessel fails explosively due to the loss of structural integrity from an impact of space debris, it can cause major damage to the equipment and a considerable amount of new space debris is created. HQP will be involved in all aspects of the work, including physical experiments and detailed numerical model development. HQP will also have the opportunity to interact with experienced satellite engineers to gain a better appreciation of the practical concerns faced by the industry with respect to satellite design. In addition to new HQP, Canadian space sector will benefit from the research outcomes of the proposed program, which will impact future satellite designs and increase their competitiveness within the industry.
轨道碎片对太空飞行安全构成重大威胁 - 由于碰撞时的速度非常高(平均约为 9 公里/秒),即使是小颗粒也可能损坏、降解或毁坏航天器。拟议研究计划的目的是在微流星体和轨道碎片(MMOD)领域开展研究工作。 ***轨道碎片的密度急剧上升,这对加拿大太空资产构成了日益增长的破坏性威胁。由于这些资产的重要性以及与其制造和部署相关的高成本,这对加拿大来说是一个战略和经济问题。由于投资规模巨大(例如 RADARSAT 星座任务计划的 1.1 亿美元合同),加拿大航天局 (CSA) 已将新的防御技术确定为加拿大航天部门的关键战略优先事项。需要改进碎片撞击建模方法(包括材料、几何和数值模型),以便卫星供应商能够研究新的防护罩配置并预测其在撞击应力下的性能。这将允许生产更耐用、寿命更长的太空飞行器,最终将延长未来加拿大太空任务的功能持续时间,造福所有加拿大人。***该研究计划的主要目标是提高我们对 MMOD 影响过程的理解。在此过程中,预计将开发出更准确的撞击行为模型,这对于卫星界开发改进的屏蔽和更耐用的卫星组件设计具有无价的价值。考虑到超高速撞击现象的复杂性和可能的​​保护解决方案的多样性,这项工作需要结合超高速撞击对盾构配置的数值和实验研究,以充分理解物理过程并显示所使用的模拟模型和方法的准确性。拟议的计划将解决一般航天器设备的保护问题,并且还将重点关注复合材料包裹压力容器的保护。当压力容器因空间碎片的撞击而失去结构完整性而发生爆炸性故障时,可能会对设备造成重大损坏,并产生大量新的空间碎片。 HQP 将参与工作的各个方面,包括物理实验和详细的数值模型开发。 HQP还将有机会与经验丰富的卫星工程师互动,以更好地了解业界在卫星设计方面面临的实际问题。除了新的总部计划外,加拿大航天部门还将受益于拟议计划的研究成果,这将影响未来的卫星设计并提高其在行业内的竞争力。

项目成果

期刊论文数量(0)
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Telichev, Igor其他文献

Influence of non-standard seating postures on safety of motorcoach passengers in frontal collisions: A numerical study
  • DOI:
    10.1016/j.ssci.2018.10.018
  • 发表时间:
    2019-03-01
  • 期刊:
  • 影响因子:
    6.1
  • 作者:
    Kuznetcov, Anton;Telichev, Igor
  • 通讯作者:
    Telichev, Igor
Weight-Efficiency of Conventional Shielding Systems in Protecting Unmanned Spacecraft from Orbital Debris
  • DOI:
    10.2514/1.a33596
  • 发表时间:
    2017-01-01
  • 期刊:
  • 影响因子:
    1.6
  • 作者:
    Cherniaev, Aleksandr;Telichev, Igor
  • 通讯作者:
    Telichev, Igor

Telichev, Igor的其他文献

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{{ truncateString('Telichev, Igor', 18)}}的其他基金

Novel Orbital Debris Protection of Spacecraft
新型航天器轨道碎片保护
  • 批准号:
    RGPIN-2018-06050
  • 财政年份:
    2022
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Discovery Grants Program - Individual
Novel Orbital Debris Protection of Spacecraft
新型航天器轨道碎片保护
  • 批准号:
    RGPIN-2018-06050
  • 财政年份:
    2021
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Discovery Grants Program - Individual
Novel Orbital Debris Protection of Spacecraft
新型航天器轨道碎片保护
  • 批准号:
    RGPIN-2018-06050
  • 财政年份:
    2020
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Discovery Grants Program - Individual
Novel Orbital Debris Protection of Spacecraft
新型航天器轨道碎片保护
  • 批准号:
    RGPIN-2018-06050
  • 财政年份:
    2019
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Discovery Grants Program - Individual
Modeling and Damage/Failure Control of Spacecraft Pressurized Structures Subject to Orbital Debris Impact
遭受轨道碎片撞击的航天器加压结构的建模和损坏/故障控制
  • 批准号:
    402115-2012
  • 财政年份:
    2017
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Discovery Grants Program - Individual
Modeling and Damage/Failure Control of Spacecraft Pressurized Structures Subject to Orbital Debris Impact
遭受轨道碎片撞击的航天器加压结构的建模和损坏/故障控制
  • 批准号:
    402115-2012
  • 财政年份:
    2016
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Discovery Grants Program - Individual
Modeling and Damage/Failure Control of Spacecraft Pressurized Structures Subject to Orbital Debris Impact
遭受轨道碎片撞击的航天器加压结构的建模和损坏/故障控制
  • 批准号:
    402115-2012
  • 财政年份:
    2015
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Discovery Grants Program - Individual
Virtual sled testing of motorcoach seat structure
客车座椅结构的虚拟雪橇测试
  • 批准号:
    474721-2014
  • 财政年份:
    2014
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Engage Grants Program
Modeling and Damage/Failure Control of Spacecraft Pressurized Structures Subject to Orbital Debris Impact
遭受轨道碎片撞击的航天器加压结构的建模和损坏/故障控制
  • 批准号:
    402115-2012
  • 财政年份:
    2014
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Discovery Grants Program - Individual
Modeling and Damage/Failure Control of Spacecraft Pressurized Structures Subject to Orbital Debris Impact
遭受轨道碎片撞击的航天器加压结构的建模和损坏/故障控制
  • 批准号:
    402115-2012
  • 财政年份:
    2013
  • 资助金额:
    $ 2.33万
  • 项目类别:
    Discovery Grants Program - Individual

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通过虚拟现实的先进轨道碎片清除技术
  • 批准号:
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  • 财政年份:
    2023
  • 资助金额:
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新型航天器轨道碎片保护
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