[求助]法国“神秘”系列战斗机资料

呵呵，没人知道吗？？？？？

晕,很老了,鸡头进气

[此贴子已经被作者于2006-7-7 13:00:27编辑过]

在82?84?年的<<国外飞机手册>>绿皮的,有较详细的叙述,以前看过.,找图书馆里应该有

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[此贴子已经被作者于2006-7-7 15:13:06编辑过]

<p>第一张......</p>

<p>Mystère IIC</p><p><br/></p><p>&nbsp;</p><p>Super Mystère</p><p><br/></p>

<p>谢谢以上朋友帮助，今天晚上把这几种加入，可以发布0.3版了。</p><p>“第一张......”，呵呵，我发的第一张图是有点“诱人”，不要想歪了。</p>[em01]

<p>神秘？记得以前《军事家》介绍过</p><p>随便贴几张</p><br/><br/><br/>

太”神秘“了 ， 没人有。

哈哈，楼主有点懒惰了，多放放狗，是可以找到很多的。

呵呵,一个人的力量还是有限的,还望朋友们能多多帮忙!

<p>Super Mystère的资料（没翻译，不过基本还是能看懂的）：</p><p>The Dassault Super Mystère French fighter-bomber was the first Western European supersonic aircraft to enter mass production.<br/>The Super Mystère represents the final step in evolution which began with Dassault Ouragan and progressed through Mystère II/III and Mystère IV. While earlier Mystère variants could attain supersonic speeds only in a dive, Super Mystère could exceed the speed of sound in level flight. This was achieved thanks to the new thin wing with 45° of sweep (compared with 41° of sweep in Mystère IV and only 33° in Mystère II) and the use of an afterburner-equipped turbojet engine. </p><p>The first prototype Super Mystère B.1, powered by Rolls-Royce Avon RA.7R, took to the air on March 2, 1955. The aircraft broke the sound barrier in level flight the following day. The aircraft entered production in 1957 as Super Mystère B.2. The production version differed from the prototype by having a more powerful SNECMA Atar 101G engine. In 1958, two Super Mystère B.4 prototypes were built. Equipped with a new 48° swept wing and a more powerful SNECMA Atar 9B engine, the aircraft were capable of Mach 1.4. Production never materialized because the faster Dassault Mirage III was entering service. In 1973, Israeli Air Force upgraded their Super Mystère B.2 with a non-afterburning version of the Pratt &amp; Whitney J52-P8A and new avionics. </p><p>A total of 180 Super Mystère B.2 were built.</p><p>Specifications (Super Mystère B.2)<br/>General characteristics<br/>Crew: One <br/>Length: 14.0 m (45 ft 11 in) <br/>Wingspan: 10.1 m (33 ft 2 in) <br/>Height: 4.6 m (15 ft 1 in) <br/>Wing area: 32.0 m&sup2; (344 ft&sup2;) <br/>Empty weight: weight: 6,390 kg (14,090 lb) <br/>Loaded weight: weight: 9,000 kg (19,800 lb) <br/>Maximum Take-Off Weight: 10,000 kg (22,000 lb) <br/>Fuel capacity: 2,000 kg (4,400 lb)) <br/>Powerplant: 1× SNECMA Atar 101G-2 turbojet, 33.3 kN dry; 44.1 kN afterburning (7,490 lbf / 9,920 lbf) <br/>Performance<br/>Maximum speed: Mach 1.12, 1,195 km/h at 11,000 m (743 mph at 36,100 ft) <br/>Range: 870 km combat, 1,175 km ferry (540 mi / 730 mi) <br/>Service ceiling: 17,000 m (55,800 ft) <br/>Rate of climb: 89 m/s (17,500 ft/min) <br/>Wing loading: 281 kg/m&sup2; (57.6 lb/ft&sup2;) <br/>Thrust/weight: 0.50 <br/>Armament<br/>2x 30 mm DEFA cannon <br/>Up to 900 kg (1,980 lb) on two wet underwing pylons, including fuel tanks, bombs, unguided rockets, MBDA AS 30 or Rafael Shafrir missiles. </p>

<p>After the success of the Ouragan, Dassault was working on a more advanced machine based on it, which would take to the air in early 1951 as the MD 452 Mystere (Mystery) I. </p><p>The first prototype Mystere I was essentially an Ouragan with a 30-degree swept wing and modified tail surfaces. Two further prototypes followed, powered by the Rolls-Royce Tay 250 centrifugal-flow turbojet, an improved version of the Rolls-Royce Nene, built under license by Hispano-Suiza, and rated at 28.0 kN (2,850 kp / 6,280 lbf) thrust. </p><p>These three Mystere I prototypes led to two Mystere IIA prototypes, powered by the Tay and armed with four Hispano 20 mm cannon; and then four Mystere IIB prototypes, which traded the four 20 millimeter cannon for two 30 millimeter DEFA revolver-type cannon. A Mystere IIA was the first French aircraft to break Mach 1 in controlled flight (in a dive), on 28 October 1951. </p><p>The eleven pre-production machines that followed were designated Mystere IIC, nine of which were fitted with the SNECMA Atar 101C axial-flow turbojet, rated at 24.5 kN (2,500 kp / 5,510 lbf) thrust, while two were experimentally fitted with the afterburning Atar 101F, with afterburning thrust of 37.3 kN (3,800 kp / 8,380 lbf).</p><p>Specifications (Mystère IIC)<br/>General characteristics<br/>Crew: One <br/>Length: 11.7 m (38 ft 6 in) <br/>Wingspan: 13.1 m (42 ft 9 in) <br/>Height: 4.26 m (14 ft) <br/>Wing area: 30.3 m&sup2; (326 ft&sup2;) <br/>Empty weight: 5,225 kg (11,520 lb) <br/>Maximum Take-Off Weight: 7,475 kg (16,480 lb) <br/>Powerplant: 1× SNECMA Atar 101D , 29.4 kN (6,615 lbf) <br/>Performance<br/>Maximum speed: 1,060 km/h (660 mph; 575 kt) <br/>Range: 885 km (550 mi; 480 nm) <br/>Service ceiling: 15,250 m (50,000 ft) <br/>Rate of climb: 23 m/s (4,530 ft/min) <br/>Wing loading: lb/ft&sup2; (kg/m&sup2;) <br/>Armament<br/>2x 30 mm DEFA cannons, 150 rounds/gun. <br/></p><p></p>