Patent ID: 11932424
Assignee: ROMAN NAWOJCZYK
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 4:
5. The system according to claim 1,
wherein the steering flaps are cardinally installed on an upper part of each space rocket fuselage by means of a plurality of hinges;
wherein each steering flap is deflected by a deflection mechanism having one linear actuator and two ample brackets;
wherein the steering flaps are adapted to steer the space rocket during its descent in the atmosphere;
wherein the steering flaps on their top parts have rotary fastened the torsional triangles which are configured to torsion-ally steer the space rocket as needed before landing on two movable gantries;
wherein each torsional triangle is grasped and axially steered by a rotary actuator fastened on the steering flaps; and
wherein the torsional triangles installing way and triangular shapes are adapted for use at various speeds of the space rocket descent in the atmosphere.