Rocket Motor with Composite Casing
The article presents the results of work concerning a two-stage rocket motor. In the first step tested stationary the charge rocket motor with the ignitor and the nozzle system in the ballistic chamber was tested. The technology of composite casing with a caliber of 171 mm, which is also a combustio...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Military University of Technology, Warsaw
2015-09-01
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| Series: | Problemy Mechatroniki |
| Subjects: | |
| Online Access: | http://publisherspanel.com/gicid/01.3001.0004.1406 |
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| _version_ | 1841563276071141376 |
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| author | Zbigniew Drabik Tomasz Rasztabiga |
| author_facet | Zbigniew Drabik Tomasz Rasztabiga |
| author_sort | Zbigniew Drabik |
| collection | DOAJ |
| description | The article presents the results of work concerning a two-stage rocket motor. In the first step tested stationary the charge rocket motor with the ignitor and the nozzle system in the ballistic chamber was tested. The technology of composite casing with a caliber of 171 mm, which is also a combustion chamber, was designed and mastered. The composite casing was tested stationary in complete rocket motor. The next step was to conduct dynamic tests at the rocket test range. During the dynamic tests
a two-stage rocket with a mass of 70 kg was fired. The rocket has reached a maximum speed of 960 m / s. |
| format | Article |
| id | doaj-art-2f17198c6fc24662a74576fa61982d99 |
| institution | Kabale University |
| issn | 2081-5891 |
| language | English |
| publishDate | 2015-09-01 |
| publisher | Military University of Technology, Warsaw |
| record_format | Article |
| series | Problemy Mechatroniki |
| spelling | doaj-art-2f17198c6fc24662a74576fa61982d992025-01-03T00:05:20ZengMilitary University of Technology, WarsawProblemy Mechatroniki2081-58912015-09-0163718410.5604/01.3001.0004.140601.3001.0004.1406Rocket Motor with Composite CasingZbigniew Drabik0Tomasz Rasztabiga1MESKO S.A. w Skarżysku-KamiennejMESKO S.A. w Skarżysku-KamiennejThe article presents the results of work concerning a two-stage rocket motor. In the first step tested stationary the charge rocket motor with the ignitor and the nozzle system in the ballistic chamber was tested. The technology of composite casing with a caliber of 171 mm, which is also a combustion chamber, was designed and mastered. The composite casing was tested stationary in complete rocket motor. The next step was to conduct dynamic tests at the rocket test range. During the dynamic tests a two-stage rocket with a mass of 70 kg was fired. The rocket has reached a maximum speed of 960 m / s.http://publisherspanel.com/gicid/01.3001.0004.1406two-stage rocketrocket motorcomposite casing |
| spellingShingle | Zbigniew Drabik Tomasz Rasztabiga Rocket Motor with Composite Casing Problemy Mechatroniki two-stage rocket rocket motor composite casing |
| title | Rocket Motor with Composite Casing |
| title_full | Rocket Motor with Composite Casing |
| title_fullStr | Rocket Motor with Composite Casing |
| title_full_unstemmed | Rocket Motor with Composite Casing |
| title_short | Rocket Motor with Composite Casing |
| title_sort | rocket motor with composite casing |
| topic | two-stage rocket rocket motor composite casing |
| url | http://publisherspanel.com/gicid/01.3001.0004.1406 |
| work_keys_str_mv | AT zbigniewdrabik rocketmotorwithcompositecasing AT tomaszrasztabiga rocketmotorwithcompositecasing |