The parameter’s optimization of the meteorological rocket’s correcting engine to reduce the zone of the used blocks’ falling
On the example of the meteorological rocket MMR-06, the optimum parameters of the trajectory correction engine to reduce the zone of the used blocks’ falling was selected. It is shown that the optimum mass and optimal maneuvering time are achieved for engines with the medium-thrust. Low-thrust engin...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
EDP Sciences
2017-01-01
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| Series: | MATEC Web of Conferences |
| Online Access: | https://doi.org/10.1051/matecconf/201712906007 |
| _version_ | 1818571803739553792 |
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| author | Mitiukov Nicholas Kasatkin Timothey Samigullina Guzalia |
| author_facet | Mitiukov Nicholas Kasatkin Timothey Samigullina Guzalia |
| author_sort | Mitiukov Nicholas |
| collection | DOAJ |
| description | On the example of the meteorological rocket MMR-06, the optimum parameters of the trajectory correction engine to reduce the zone of the used blocks’ falling was selected. It is shown that the optimum mass and optimal maneuvering time are achieved for engines with the medium-thrust. Low-thrust engines, despite the minimum weight, provide a long maneuver time and because of their large number, the total mass increases. The large-thrust engines are very heavy and capable of causing dangerous lateral overloads. |
| first_indexed | 2024-12-14T18:49:09Z |
| format | Article |
| id | doaj.art-873a40875fd9468db1566c495fa79b0e |
| institution | Directory Open Access Journal |
| issn | 2261-236X |
| language | English |
| last_indexed | 2024-12-14T18:49:09Z |
| publishDate | 2017-01-01 |
| publisher | EDP Sciences |
| record_format | Article |
| series | MATEC Web of Conferences |
| spelling | doaj.art-873a40875fd9468db1566c495fa79b0e2022-12-21T22:51:19ZengEDP SciencesMATEC Web of Conferences2261-236X2017-01-011290600710.1051/matecconf/201712906007matecconf_icmtmte2017_06007The parameter’s optimization of the meteorological rocket’s correcting engine to reduce the zone of the used blocks’ fallingMitiukov NicholasKasatkin TimotheySamigullina GuzaliaOn the example of the meteorological rocket MMR-06, the optimum parameters of the trajectory correction engine to reduce the zone of the used blocks’ falling was selected. It is shown that the optimum mass and optimal maneuvering time are achieved for engines with the medium-thrust. Low-thrust engines, despite the minimum weight, provide a long maneuver time and because of their large number, the total mass increases. The large-thrust engines are very heavy and capable of causing dangerous lateral overloads.https://doi.org/10.1051/matecconf/201712906007 |
| spellingShingle | Mitiukov Nicholas Kasatkin Timothey Samigullina Guzalia The parameter’s optimization of the meteorological rocket’s correcting engine to reduce the zone of the used blocks’ falling MATEC Web of Conferences |
| title | The parameter’s optimization of the meteorological rocket’s correcting engine to reduce the zone of the used blocks’ falling |
| title_full | The parameter’s optimization of the meteorological rocket’s correcting engine to reduce the zone of the used blocks’ falling |
| title_fullStr | The parameter’s optimization of the meteorological rocket’s correcting engine to reduce the zone of the used blocks’ falling |
| title_full_unstemmed | The parameter’s optimization of the meteorological rocket’s correcting engine to reduce the zone of the used blocks’ falling |
| title_short | The parameter’s optimization of the meteorological rocket’s correcting engine to reduce the zone of the used blocks’ falling |
| title_sort | parameter s optimization of the meteorological rocket s correcting engine to reduce the zone of the used blocks falling |
| url | https://doi.org/10.1051/matecconf/201712906007 |
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