| 摘要 |
The utility model relates to the rocket-space branch. A rocket nose fairing contains conical and cylindrical sections divided by means of longitudinal joint into the flaps, longitudinal auxiliary joints with hinges made inside each fold of cylindrical section, a dump system and locks installed in the longitudinal joint on the internal surface of folds, which consist of the holders with spring-loaded pins fixed on one flap, and the fittings fixed on the second flap and which interact with the spring-loaded pins. For increasing the operating characteristics the spring-loaded pins are located in parallel with longitudinal axis of the nose fairing and oriented to the side of its tip.
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