FIELD: machine engineering.
SUBSTANCE: capacity of the composite material comprises structural envelope formed with mating shell bottoms and interface unit located in the bottom zone of coupling with the shell. Wherein the interface unit to the power generated taped shell packets and the composite material comprises a metal made of a valve fastening, the frame and formed by a power shaft. The shank is designed as a ring fastened to the power frame longitudinal webs, and bonded to the ring longitudinal tabs. In this ring and longitudinal bridges longitudinal tabs are located between the main hull and the composite packets.
EFFECT: weight reduction and interface unit length.
6 cl, 4 dwg
Title | Year | Author | Number |
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HOUSING OF SOLID-PROPELLANT ROCKET ENGINE | 2003 |
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RU2237186C1 |
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|
RU2189162C2 |
Authors
Dates
2017-05-11—Published
2016-04-19—Filed