| 摘要 |
FIELD: transport. ^ SUBSTANCE: invention is used in the hypersonic aircraft flight control system when operating in dense atmosphere. The unit includes a thermal airframe, stabilisation system instrument unit, flight path assignment unit, onboard computational facility with input-output unit, m-unit comprising the actuating elements for changing the aircraft aerodynamic qualities and n-unit (n >= m) comprising material ablation sensors. The sensing elements of the ablation sensors are mounted in the ablating material of the thermal airframe. ^ EFFECT: reduced initial mass of ablating material and improved aerodynamic qualities of the aircraft. ^ 2 dwg |
