FIELD: rocketry.
SUBSTANCE: proposed solid-propellant rocket engine includes channel charge secured to case and to end faces by means of collars which have bulges in their necks. Size of this bulge is 1.5-2.5 of collar thickness along generatrix of neck at neck outlet. Angle formed by bulge surface directed to propellant and axis of charge channel ranges from 45 to 90 deg.
EFFECT: maximum volume occupied by propellant; avoidance of defects in charging.
4 dwg
Title |
Year |
Author |
Number |
OUTFITTED SOLID-PROPELLANT ROCKET ENGINE HOUSING |
2009 |
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|
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SOLID-PROPELLANT ROCKET ENGINE HOUSING |
2018 |
- Bondarenko Sergej Aleksandrovich
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- Krasnyshev Maksim Viktorovich
- Gabov Ilya Aleksandrovich
- Budnikov Vitalij Viktorovich
|
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LOADED CASE OF SOLID PROPELLANT ROCKET ENGINE |
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|
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SOLID-PROPELLANT ROCKET |
2012 |
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|
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2016 |
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|
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2002 |
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