| 摘要 |
FIELD: rocket engineering. SUBSTANCE: nose section has body, nose fairing, parachute system and ejection charge. Nose fairing carries cylindrical shell located inside body. Face part of body has rest on side of fairing interacting with external surface of shell. Piston interacting with internal and face surfaces of shell is placed between parachute system and ejection charge. Outer cylindrical surface of piston interacts with inner surface of body. Parachute system is located inside nose fairing and is attached to piston. EFFECT: enhanced reliability of setting parachute system in action while heavy dynamic pressure head of air acts on rocket. 2 cl, 1 dwg
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