DEVICE FOR SEPARATION OF NOSE OF CARRIER ROCKET Russian patent published in 2004 - IPC

FIELD: space equipment, applicable for separation of dropped nose cone of carrier rocket.

SUBSTANCE: the device has a pusher including a sleeve and a stop with an eye secured on a bracket by means of a pin, spring-loaded flange, tailpiece engageable with the support and the central rod with a ring spread positioned inside the sleeve - all fastened on the carrier rocket for rotation of the flap. Each pusher is installed on the outer surface of the flaps for deflection, provided with a housing and a damper, the central rod is rigidly fastened to the flange with the tailpiece installed on its opposite side for adjustment of its axial position. The sleeve is made with an inner ring boss. The outer surface of the ring spread of the central rod is engageable with the inner surface of the sleeve. The housing is made for enveloping the flange outer surface. The damper is installed on the central rod between its ring spread and the inner ring boss of the flange. The stop is provided with a pin rocker bearing fastened in its eye by an outer ring, and on the pin-by an inner ring. The central rod is installed for fixation relative to the stop. The bracket is provided with a local fairing. The support is fastened on the carrier rocket. The pin axis is parallel with the axis of flap rotation, and the tailpiece is made with a spherical tip.

EFFECT: enhanced reliability of separation of the nose cone.

3 dwg