FIELD: transport.
SUBSTANCE: invention relates to rocketry. Proposed shuttlecraft comprises fuselage, with two outer wings, left and right control engines. Said outer wings are equipped with tips. Control engines left and right units are arranged in nacelles at outer wing tips to allow application of control engines at ascent and descent paths. Axes pitch and bank control engine nozzles are parallel with shuttlecraft normal axis OY. Engine nozzle yaw axes are perpendicular to said normal axis OY to make therewith angle φ equal to 0°…20°.
EFFECT: better shuttlecraft controllability.
5 dwg
