FIELD: space engineering. SUBSTANCE: method consists in withdrawal of parachute from container by imparting preset velocity to structural members relative to re-entry vehicle along its longitudinal axis due to force of separation system; preset velocity is imparted to structural members of parachute by motion of container relative to re-entry space vehicle; magnitude of force of separation system acting on parachute container is found from relationship given in Description. EFFECT: enhanced reliability. 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DESCENT SPACE VEHICLE | 1993 |
|
RU2092406C1 |
| RE-ENTRY CAPSULE | 1992 |
|
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| DEVICE FOR DROPPING HEAVY LOADS FROM FLYING VEHICLES | 1992 |
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| LIGHT PROTECTIVE DEVICE FOR SPACE VEHICLE | 1995 |
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| THREE-LINE HYDRAULIC DISTRIBUTOR | 1991 |
|
RU2111895C1 |
