【流星空空導彈】歐洲六國驚世之作，作戰性能遠超各國現役空空導彈？一枚200萬歐元，曾擊落F22戰鬥機，卻存在明顯的硬傷 скачать в хорошем качестве

【流星空空導彈】歐洲六國驚世之作，作戰性能遠超各國現役空空導彈？一枚200萬歐元，曾擊落F22戰鬥機，卻存在明顯的硬傷

“流星”空空導彈是以吸氣式發動機為動力的新一代空空導彈。該彈採用了主動尋的雷達導引頭及雙向數據鏈技術，發動機燃氣流量調節比大於10，具有相當寬的飛行包線。通過對該彈的各項性能的分析，可以確定“流星”導彈的整體作戰性能將超過世界各國現役的各型中程空空導彈。 導彈採用固體火箭沖壓發動機和彈載脈衝多普勒雷達，具有全天候攻擊能力，在相當廣的空域內具有同時對付多個目標的能力，即使目標做8～9G的機動過載，“流星”依然能夠跟踪到目標並將其摧毀。該彈的主要載機為“陣風”、“颱風”、“鷹獅”等戰鬥機，攻擊目標包括戰鬥機、轟炸機、預警機等在內的空中目標。 導彈全長為3.65米，彈徑180毫米，發射重量為185千克，動力裝置為可變流量的固體火箭沖壓發動機，採用雙下側二元進氣道，彈體中部有兩片彈翼。彈體主要由導引頭天線罩、電子系統艙、戰鬥部艙以及整體式固體火箭發動機艙4部分組成。數據鏈接收機安裝在兩個進氣道之間，數據鏈天線則安裝在彈體的尾部。導彈採用正常的氣動佈局，靜穩定尾翼控制，進氣道間隔為90。徑向角，呈面對稱配置。 4片全動式梯形尾舵、2片固定彈翼，與二元進氣道一起呈軸對稱配置。 2003年設計小組更改了設計方案，將原先設置在彈體中部的2片彈翼取消，同時減小了彈體尾部的4片尾舵的面積，這樣整枚導彈看上去更加簡練，其飛行速度也將有所提高。 The "Meteor" air-to-air missile is a new generation of air-to-air missile powered by aspirated engines. The missile uses an active homing radar seeker and two-way data link technology, the engine gas flow regulation ratio is greater than 10, and has a fairly wide flight envelope. Through the analysis of the various performances of the bomb, it can be determined that the overall combat performance of the "Meteor" missile will exceed the various types of medium-range air-to-air missiles currently in service in various countries around the world. The missile uses a solid rocket ramjet and a missile-borne pulse Doppler radar. It has all-weather attack capability and the ability to simultaneously deal with multiple targets in a relatively wide airspace. Even if the target is maneuvered over 8 to 9G, the "Meteor" can still be used. Track the target and destroy it. The main carriers of the bomb are fighters such as Rafale, Typhoon, and Gripen, and its attack targets include fighters, bombers, early warning aircraft, and other aerial targets. The missile has a total length of 3.65 meters, a projectile diameter of 180 millimeters, and a launch weight of 185 kilograms. The power unit is a solid rocket ramjet with a variable flow rate. It uses dual lower side dual air inlets and has two missile wings in the middle of the projectile. The missile body is mainly composed of the seeker radome, the electronic system cabin, the warhead cabin and the integral solid rocket engine cabin. The data link receiver is installed between the two air inlets, and the data link antenna is installed on the tail of the projectile. The missile adopts the normal aerodynamic layout, statically stable tail control, and the air inlet interval is 90. Radial angle, symmetrical configuration. 4 full-moving trapezoidal rudders and 2 fixed missile wings are arranged axisymmetrically with the binary air inlet. In 2003, the design team changed the design plan by canceling the two wings that were originally set in the middle of the missile body. At the same time, the area of ​​the four tail rudders at the tail of the missile body was reduced, so that the whole missile looks more concise and its flight speed is also Will be improved.