Solving an irregular burning problem in a small rocket motor
During the design and development of a solid rocket motor, intensive irregular burning appeared in the area of high initial temperatures. The cylindrical propellant grain was designed for approximately neutral burning, with a hollow tube and both burning ends as well as with the outer surface inhibi...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Military Technical Institute, Belgrade
2014-01-01
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| Series: | Scientific Technical Review |
| Subjects: | |
| Online Access: | https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2014/1820-02061402003G.pdf |