发明名称 |
DEVICE FOR AIRFLOW CONTROL OF HYPERSONIC FLYING VEHICLE |
摘要 |
FIELD: rocketry and space engineering. ^ SUBSTANCE: proposed device has nose section 1 and central and additional aerodynamic needles 3 made in form of thin cylindrical rods which are stowed in special passages made in nose section of flying vehicle. One passage is located along axis of symmetry and other passages are located at some distance from axis of symmetry smoothly over circumference whose center lies at axis of symmetry. Each passage is provided with mechanism for delivery of aerodynamic needles towards incoming flow; provision is made for extension of each needle through definite length for forming special configuration of set of needles which is necessary for their joint operation in airflow control. ^ EFFECT: possibility of obtaining constant coordinate of center of pressure of hypersonic flying vehicle; reduced force of drag; possibility of forming control forces and moments for manoeuvring in atmosphere. ^ 4 dwg |
申请公布号 |
RU2268847(C1) |
申请公布日期 |
2006.01.27 |
申请号 |
RU20040116169 |
申请日期 |
2004.05.27 |
申请人 |
|
发明人 |
TIPAEV VLADIMIR VLADIMIROVICH;NIKITIN KONSTANTIN VLADIMIROVICH;PIROGOV SERGEJ JUR'EVICH;MOSKALETS GENNADIJ NIKOLAEVICH;JUR'EV ANATOLIJ STEPANOVICH |
分类号 |
B64G1/22;B64C21/00;B64C23/06;B64G1/46 |
主分类号 |
B64G1/22 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|