| abstract |
FIELD: aircraft engineering. SUBSTANCE: flying vehicle has front compartment 1 with a television position indicator, a date correlation processing unit and four destabilizers 2 X-like mounted on the compartment, additional thin-walled adapter compartment 3 with self-centering locking mechanism 4 and detachable shroud 5, useful load compartment 6 with actuating mechanism 7 and aft compartment 8 with a control system unit, a turbogenerator power source and four stabilizers 9 with aerodynamic control surfaces 10, the stabilizers are X-like fastened to the power source. All compartments are connected in series. Exhaust branch pipes of turbogenerator 11 are symmetrically brought out between side stabilizers. EFFECT: improved structure. 4 cl, 2 dwg |