Stratospheric effects of rocket launch emissions.

The rate of rocket launches around the world is accelerating, driven by the rapid global development of the space industry. However, the cumulative effects of orbital launch vehicle emissions on the stratosphere are poorly understood. Individual rocket launches deposit potentially significant quanti...

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Main Author: Brown, Tyler F. M.
Format: Thesis
Language:English
Published: 2022
Subjects:
Online Access:https://hdl.handle.net/10092/104007
https://doi.org/10.26021/13105
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spelling ftunivcanter:oai:ir.canterbury.ac.nz:10092/104007 2024-09-15T17:48:07+00:00 Stratospheric effects of rocket launch emissions. Brown, Tyler F. M. 2022 application/pdf https://hdl.handle.net/10092/104007 https://doi.org/10.26021/13105 English en eng https://hdl.handle.net/10092/104007 http://dx.doi.org/10.26021/13105 All Rights Reserved https://canterbury.libguides.com/rights/theses Theses / Dissertations 2022 ftunivcanter https://doi.org/10.26021/13105 2024-07-24T23:44:54Z The rate of rocket launches around the world is accelerating, driven by the rapid global development of the space industry. However, the cumulative effects of orbital launch vehicle emissions on the stratosphere are poorly understood. Individual rocket launches deposit potentially significant quantities of soot, alumina, nitrogen oxides, reactive chlorine, carbon dioxide, and water vapor into the stratosphere. To address this, a new inventory is created to catalogue the per-vehicle contributions to stratospheric emissions of the launch industry, referenced to 2019. All major fuel types currently used are included in the dataset in order to generate an aggregate of the above listed emission species. The dataset is used in simulation of a heavy future launch cadence scenario (2,040 launches/year) based on year 2030 conditions using the SOCOLv4 chemistry-climate model. An overall 0.5% decrease in average global total column ozone is found due to rocket launch emissions. Antarctic (60-90◦S) springtime total column ozone is reduced by 9 DU (-3.8%). Arctic (60-90◦N) springtime ozone is reduced by 11 DU (-2.4%), which is equivalent to half of the springtime ozone loss seen over this region due to chlorofluorocarbons in the late 20th century. O₃ depletion is largely chlorine based, as alumina and black carbon particulates are not quantified in this simulation. Rocket launch emission effects of this scale imply additionally delayed recovery of the ozone layer by up to a decade. Selected current environmental regulation and space policy are also summarized; they largely omit stratospheric effects of rocket activity. These findings reiterate the need for international cooperation and contextualization of emissions systems in which individual actors have comparatively widespread impact. Thesis Antarc* Antarctic black carbon University of Canterbury, Christchurch: UC Research Repository
institution Open Polar
collection University of Canterbury, Christchurch: UC Research Repository
op_collection_id ftunivcanter
language English
description The rate of rocket launches around the world is accelerating, driven by the rapid global development of the space industry. However, the cumulative effects of orbital launch vehicle emissions on the stratosphere are poorly understood. Individual rocket launches deposit potentially significant quantities of soot, alumina, nitrogen oxides, reactive chlorine, carbon dioxide, and water vapor into the stratosphere. To address this, a new inventory is created to catalogue the per-vehicle contributions to stratospheric emissions of the launch industry, referenced to 2019. All major fuel types currently used are included in the dataset in order to generate an aggregate of the above listed emission species. The dataset is used in simulation of a heavy future launch cadence scenario (2,040 launches/year) based on year 2030 conditions using the SOCOLv4 chemistry-climate model. An overall 0.5% decrease in average global total column ozone is found due to rocket launch emissions. Antarctic (60-90◦S) springtime total column ozone is reduced by 9 DU (-3.8%). Arctic (60-90◦N) springtime ozone is reduced by 11 DU (-2.4%), which is equivalent to half of the springtime ozone loss seen over this region due to chlorofluorocarbons in the late 20th century. O₃ depletion is largely chlorine based, as alumina and black carbon particulates are not quantified in this simulation. Rocket launch emission effects of this scale imply additionally delayed recovery of the ozone layer by up to a decade. Selected current environmental regulation and space policy are also summarized; they largely omit stratospheric effects of rocket activity. These findings reiterate the need for international cooperation and contextualization of emissions systems in which individual actors have comparatively widespread impact.
format Thesis
author Brown, Tyler F. M.
spellingShingle Brown, Tyler F. M.
Stratospheric effects of rocket launch emissions.
author_facet Brown, Tyler F. M.
author_sort Brown, Tyler F. M.
title Stratospheric effects of rocket launch emissions.
title_short Stratospheric effects of rocket launch emissions.
title_full Stratospheric effects of rocket launch emissions.
title_fullStr Stratospheric effects of rocket launch emissions.
title_full_unstemmed Stratospheric effects of rocket launch emissions.
title_sort stratospheric effects of rocket launch emissions.
publishDate 2022
url https://hdl.handle.net/10092/104007
https://doi.org/10.26021/13105
genre Antarc*
Antarctic
black carbon
genre_facet Antarc*
Antarctic
black carbon
op_relation https://hdl.handle.net/10092/104007
http://dx.doi.org/10.26021/13105
op_rights All Rights Reserved
https://canterbury.libguides.com/rights/theses
op_doi https://doi.org/10.26021/13105
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