Jarrod Moonen , Andrea Mazzanti , Jafar Shojaii , Simon Barter , Shannon Ryan , Crystal Forrester , Pier Marzocca , Alex Shekhter
{"title":"多功能高强低z复合材料在近地轨道上屏蔽电离粒子的能力","authors":"Jarrod Moonen , Andrea Mazzanti , Jafar Shojaii , Simon Barter , Shannon Ryan , Crystal Forrester , Pier Marzocca , Alex Shekhter","doi":"10.1016/j.actaastro.2025.08.055","DOIUrl":null,"url":null,"abstract":"<div><div>The ionization shielding performance of orbital debris (OD) shields, containing Ultrahigh Molecular Weight Polyethylene (UHMWPE) and aramid, have been investigated. We report the SRIM-2013 numerical simulation of the protons and heavy ions interaction with the shield, based on the description of the orbital ion environment for the analogue satellite NOVASAR-1, validated by experimentation at the Australia National University’s Heavy Ion Accelerator Facility Space Radiation Beamline. The suitability of the structures as ionizing radiation shields were measured on two metrics induced in a notional commercial-off-the-shelf (COTS) Integrated Circuit chip (IC) and Radiation Hardened (RH) IC relative to a no-shield baseline: (1) change in Soft Error Rate (SER) using SER cross-section data for chip architectures published in literature, and (2) change in Total Ionizing Dose (TID) over a notional mission time frame. The analysis finds the all considered shields increase the SER for the RH chip architecture by approx. 20%, while an approx. 1.5% drop in SER independent of the shield constituent materials analysed was predicted in the COTS case. A significant drop in TID (68%–83%) was predicted due to the presence of a shielding structure, with the UHMWPE shield outperforming the aramid shield by a functionally negligible 2%.</div></div>","PeriodicalId":44971,"journal":{"name":"Acta Astronautica","volume":"238 ","pages":"Pages 598-607"},"PeriodicalIF":3.4000,"publicationDate":"2025-09-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"The ionizing particle shielding capability of multi-functional high-strength and low-Z composites in low earth orbit\",\"authors\":\"Jarrod Moonen , Andrea Mazzanti , Jafar Shojaii , Simon Barter , Shannon Ryan , Crystal Forrester , Pier Marzocca , Alex Shekhter\",\"doi\":\"10.1016/j.actaastro.2025.08.055\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The ionization shielding performance of orbital debris (OD) shields, containing Ultrahigh Molecular Weight Polyethylene (UHMWPE) and aramid, have been investigated. We report the SRIM-2013 numerical simulation of the protons and heavy ions interaction with the shield, based on the description of the orbital ion environment for the analogue satellite NOVASAR-1, validated by experimentation at the Australia National University’s Heavy Ion Accelerator Facility Space Radiation Beamline. The suitability of the structures as ionizing radiation shields were measured on two metrics induced in a notional commercial-off-the-shelf (COTS) Integrated Circuit chip (IC) and Radiation Hardened (RH) IC relative to a no-shield baseline: (1) change in Soft Error Rate (SER) using SER cross-section data for chip architectures published in literature, and (2) change in Total Ionizing Dose (TID) over a notional mission time frame. The analysis finds the all considered shields increase the SER for the RH chip architecture by approx. 20%, while an approx. 1.5% drop in SER independent of the shield constituent materials analysed was predicted in the COTS case. A significant drop in TID (68%–83%) was predicted due to the presence of a shielding structure, with the UHMWPE shield outperforming the aramid shield by a functionally negligible 2%.</div></div>\",\"PeriodicalId\":44971,\"journal\":{\"name\":\"Acta Astronautica\",\"volume\":\"238 \",\"pages\":\"Pages 598-607\"},\"PeriodicalIF\":3.4000,\"publicationDate\":\"2025-09-19\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Acta Astronautica\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0094576525005636\",\"RegionNum\":2,\"RegionCategory\":\"物理与天体物理\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Acta Astronautica","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0094576525005636","RegionNum":2,"RegionCategory":"物理与天体物理","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
The ionizing particle shielding capability of multi-functional high-strength and low-Z composites in low earth orbit
The ionization shielding performance of orbital debris (OD) shields, containing Ultrahigh Molecular Weight Polyethylene (UHMWPE) and aramid, have been investigated. We report the SRIM-2013 numerical simulation of the protons and heavy ions interaction with the shield, based on the description of the orbital ion environment for the analogue satellite NOVASAR-1, validated by experimentation at the Australia National University’s Heavy Ion Accelerator Facility Space Radiation Beamline. The suitability of the structures as ionizing radiation shields were measured on two metrics induced in a notional commercial-off-the-shelf (COTS) Integrated Circuit chip (IC) and Radiation Hardened (RH) IC relative to a no-shield baseline: (1) change in Soft Error Rate (SER) using SER cross-section data for chip architectures published in literature, and (2) change in Total Ionizing Dose (TID) over a notional mission time frame. The analysis finds the all considered shields increase the SER for the RH chip architecture by approx. 20%, while an approx. 1.5% drop in SER independent of the shield constituent materials analysed was predicted in the COTS case. A significant drop in TID (68%–83%) was predicted due to the presence of a shielding structure, with the UHMWPE shield outperforming the aramid shield by a functionally negligible 2%.
期刊介绍:
Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to:
The peaceful scientific exploration of space,
Its exploitation for human welfare and progress,
Conception, design, development and operation of space-borne and Earth-based systems,
In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.