FIELD: rocketry, applicable in construction of rockets provided with a device for separation of electrical communications of the rocket with the transport-launching pack.
SUBSTANCE: the device for separation is positioned in the longitudinal plane of the rocket symmetry and made in the form of two symmetrically positioned torsion springs installed in the axis in a recess of the pack body. One end of each spring is connected to the pack body, and the other is L-shaped located perpendicularly to the rocket longitudinal axis between the pack body and the rocket, with the arm bent in the direction of rocket motion and rigidly connected to the electrical connector receptacle. The recess in the pack body is made in the direction of the rocket nose according to the dimensions of the device for separation with the separated electrical connector receptacle.
EFFECT: enhanced reliability of the device for separation of the electrical connector receptacles.
5 dwg
| Title | Year | Author | Number |
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|
RU2302600C1 |
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|
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| LAUNCHING SYSTEM | 2009 |
|
RU2406961C1 |
