发明名称 |
УСТРОЙСТВО ДЛЯ УПРАВЛЕНИЯ ПОЛЕТОМ ГИПЕРЗВУКОВОГО ЛЕТАТЕЛЬНОГО АППАРАТА |
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 |
申请公布号 |
RU2005127946(A) |
申请公布日期 |
2007.03.20 |
申请号 |
RU20050127946 |
申请日期 |
2005.09.08 |
申请人 |
Серпуховской военный институт ракетных войск (СВИРВ) (RU);Межрегиональное общественное учреждение "Институтинженерной физики" (МОУ "ИИФ") (RU) |
发明人 |
Коробков Алексей Александрович (RU);Смирнов Дмитрий В чеславович (RU);Мурашко Игорь Анатольевич (RU) |
分类号 |
B64C19/00 |
主分类号 |
B64C19/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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