TWO-STAGE ROLLING ROCKET Russian patent published in 1998 - IPC

Abstract RU 2110755 C1

FIELD: two-stage rolling rocket. SUBSTANCE: a stabilizer with an oblique tail unit is installed on the rocket acceleration engine. The tail unit of the rocket head stage is installed relative to the longitudinal axis at an angle smaller than the angle of turn of stabilizing fins. The trailing edges of the head stage tail unit fins are located in grooves made in the front part of the intermediate cone. EFFECT: enhanced reliability. 3 dwg

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RU 2 110 755 C1

Authors

Zhukov V.P.

Kuznetsov V.M.

Khripunov L.A.

Dates

1998-05-10Published

1996-01-09Filed