【News】减少F-35性能规格可能产生重大的作战影响

来源:百度文库 编辑:超级军网 时间:2024/04/30 05:23:31


Reduced F-35 performance specifications may have significant operational impact

By:   Dave Majumdar Washington DC


The Pentagon's decision to reduce the performance specifications for the Lockheed Martin F-35 Joint Strike Fighter will have a significant operational impact, a number of highly experienced fighter pilots consulted by Flightglobal concur. But the careful development of tactics and disciplined employment of the jet may be able to mitigate some of those shortcomings.

"This is going to have a big tactical impact," one highly experienced officer says. "Anytime you have to lower performance standards, the capability of what the airframe can do goes down as well."



The US Department of Defense's decision to relax the sustained turn performance of all three variants of the F-35 was revealed earlier this month in the Pentagon's Director of Operational Test and Evaluation 2012 report. Turn performance for the US Air Force's F-35A was reduced from 5.3 sustained g's to 4.6 sustained g's. The F-35B had its sustained g's cut from five to 4.5 g's, while the US Navy variant had its turn performance truncated from 5.1 to five sustained g's. Acceleration times from Mach 0.8 to Mach 1.2 were extended by eight seconds, 16 seconds and 43 seconds for the A, B and C-models respectively. The baseline standard used for the comparison was a clean Lockheed F-16 Block 50 with two wingtip Raytheon AIM-120 AMRAAMs. "What an embarrassment, and there will be obvious tactical implications. Having a maximum sustained turn performance of less than 5g is the equivalent of an [McDonnell Douglas] F-4 or an [Northrop] F-5," another highly experienced fighter pilot says. "[It's] certainly not anywhere near the performance of most fourth and fifth-generation aircraft."

At higher altitudes, the reduced performance will directly impact survivability against advanced Russian-designed "double-digit" surface-to-air missile (SAM) systems such as the Almaz-Antey S-300PMU2 (also called the SA-20 Gargoyle by the North Atlantic Treaty Organization), the pilot says. At lower altitudes, where fighters might operate in for the close air support or forward air control role, the reduced airframe performance will place pilots at increased risk against shorter-range SAMs and anti-aircraft artillery.

Most egregious is the F-35C-model's drastically reduced transonic acceleration capabilities. "That [43 seconds] is a massive amount of time, and assuming you are in afterburner for acceleration, it's going to cost you even more gas," the pilot says. "This will directly impact tactical execution, and not in a good way."

Pilots typically make the decision to trade a very high rate of fuel consumption for supersonic airspeeds for one of two reasons. "They are either getting ready to kill something or they are trying to defend against something [that's trying to kill] them," the pilot says. "Every second counts in both of those scenarios. The longer it takes, the more compressed the battle space gets. That is not a good thing."



While there is no disputing that the reduced performance specifications are a negative development, there may be ways to make up for some of the F-35's less than stellar kinematic performance.

Pilots will have to make extensive use of the F-35's stealth characteristics and sensors to compensate for performance areas where the jet has weaknesses, sources familiar with the aircraft say. But engagement zones and maneuvering ranges will most likely be driven even further out against the most dangerous surface-to-air threats.

In an air-to-air engagement, for example, tactics would have to be developed to emphasize stealth and beyond visual range (BVR) combat. If a visual range engagement is unavoidable, every effort would have to be taken to enter the "merge" from a position of advantage, which should be possible, given the F-35's stealth characteristics.

Once engaged within visual range, given the F-35's limitations and relative strengths, turning should be minimized in favor of using the jet's Northrop Grumman AAQ-37 distributed aperture system of infrared cameras, helmet-mounted display and high off-boresight missiles to engage the enemy aircraft. If a turning fight is unavoidable, the F-35 has good instantaneous turn performance and good high angle of attack (50°AOA limit) performance comparable to a Boeing F/A-18 Hornet, which means a similar strategy could be adopted if one finds him or herself in such a situation.


Lockheed, for its part, maintains that the F-35 has performance superior to that of any "legacy" fighter at high altitudes. "Having flown over 4000 hours in fighter jets, I will tell you the F-35's capability at altitude, mostly driven by the internal carriage of those weapons, as a combat airplane, this airplane exceeds the capabilities of just any legacy fighter that I'm familiar with in this kind of regime," says Steve O'Bryan, the company's business development director for the F-35 during a January interview.

But much of the discussion is theoretical at this point, the F-35 has not been operationally tested, nor have tactics been developed for the aircraft's usage. How the aircraft will eventually fare once fully developed and fielded is an open question.


http://www.flightglobal.com/news ... onal-impact-381683/


Reduced F-35 performance specifications may have significant operational impact

By:   Dave Majumdar Washington DC


The Pentagon's decision to reduce the performance specifications for the Lockheed Martin F-35 Joint Strike Fighter will have a significant operational impact, a number of highly experienced fighter pilots consulted by Flightglobal concur. But the careful development of tactics and disciplined employment of the jet may be able to mitigate some of those shortcomings.

"This is going to have a big tactical impact," one highly experienced officer says. "Anytime you have to lower performance standards, the capability of what the airframe can do goes down as well."



The US Department of Defense's decision to relax the sustained turn performance of all three variants of the F-35 was revealed earlier this month in the Pentagon's Director of Operational Test and Evaluation 2012 report. Turn performance for the US Air Force's F-35A was reduced from 5.3 sustained g's to 4.6 sustained g's. The F-35B had its sustained g's cut from five to 4.5 g's, while the US Navy variant had its turn performance truncated from 5.1 to five sustained g's. Acceleration times from Mach 0.8 to Mach 1.2 were extended by eight seconds, 16 seconds and 43 seconds for the A, B and C-models respectively. The baseline standard used for the comparison was a clean Lockheed F-16 Block 50 with two wingtip Raytheon AIM-120 AMRAAMs. "What an embarrassment, and there will be obvious tactical implications. Having a maximum sustained turn performance of less than 5g is the equivalent of an [McDonnell Douglas] F-4 or an [Northrop] F-5," another highly experienced fighter pilot says. "[It's] certainly not anywhere near the performance of most fourth and fifth-generation aircraft."

At higher altitudes, the reduced performance will directly impact survivability against advanced Russian-designed "double-digit" surface-to-air missile (SAM) systems such as the Almaz-Antey S-300PMU2 (also called the SA-20 Gargoyle by the North Atlantic Treaty Organization), the pilot says. At lower altitudes, where fighters might operate in for the close air support or forward air control role, the reduced airframe performance will place pilots at increased risk against shorter-range SAMs and anti-aircraft artillery.

Most egregious is the F-35C-model's drastically reduced transonic acceleration capabilities. "That [43 seconds] is a massive amount of time, and assuming you are in afterburner for acceleration, it's going to cost you even more gas," the pilot says. "This will directly impact tactical execution, and not in a good way."

Pilots typically make the decision to trade a very high rate of fuel consumption for supersonic airspeeds for one of two reasons. "They are either getting ready to kill something or they are trying to defend against something [that's trying to kill] them," the pilot says. "Every second counts in both of those scenarios. The longer it takes, the more compressed the battle space gets. That is not a good thing."



While there is no disputing that the reduced performance specifications are a negative development, there may be ways to make up for some of the F-35's less than stellar kinematic performance.

Pilots will have to make extensive use of the F-35's stealth characteristics and sensors to compensate for performance areas where the jet has weaknesses, sources familiar with the aircraft say. But engagement zones and maneuvering ranges will most likely be driven even further out against the most dangerous surface-to-air threats.

In an air-to-air engagement, for example, tactics would have to be developed to emphasize stealth and beyond visual range (BVR) combat. If a visual range engagement is unavoidable, every effort would have to be taken to enter the "merge" from a position of advantage, which should be possible, given the F-35's stealth characteristics.

Once engaged within visual range, given the F-35's limitations and relative strengths, turning should be minimized in favor of using the jet's Northrop Grumman AAQ-37 distributed aperture system of infrared cameras, helmet-mounted display and high off-boresight missiles to engage the enemy aircraft. If a turning fight is unavoidable, the F-35 has good instantaneous turn performance and good high angle of attack (50°AOA limit) performance comparable to a Boeing F/A-18 Hornet, which means a similar strategy could be adopted if one finds him or herself in such a situation.


Lockheed, for its part, maintains that the F-35 has performance superior to that of any "legacy" fighter at high altitudes. "Having flown over 4000 hours in fighter jets, I will tell you the F-35's capability at altitude, mostly driven by the internal carriage of those weapons, as a combat airplane, this airplane exceeds the capabilities of just any legacy fighter that I'm familiar with in this kind of regime," says Steve O'Bryan, the company's business development director for the F-35 during a January interview.

But much of the discussion is theoretical at this point, the F-35 has not been operationally tested, nor have tactics been developed for the aircraft's usage. How the aircraft will eventually fare once fully developed and fielded is an open question.


http://www.flightglobal.com/news ... onal-impact-381683/
也不翻译一下。。。
binglayueshe 发表于 2013-1-31 11:26
也不翻译一下。。。
韩文的日文的我翻译了,英文应该不需要吧。。
方言增加阅读障碍呀。
回头有时间给大家大概翻译一下。。现在上班没时间 sorry~
头一次看夜晚的编队灯,很漂亮!
反鸟语神教何在!
35的背部不错,腹部真心不好看
肥电的腹部设计违反人类的普遍审美观念。


大致翻译了一下,就是按照原文翻译的,水平有限,见谅、、、
PS,长时间不用英文,水平下降的很厉害。。。改了几个错别字

    许多具有丰富经验的战斗机飞行员被咨询时认为,五角大楼决定降低肥电的性能参数会带来重大的操作上的冲击。但是细致的战术和航空雇员的纪律可以减少这些缺点。
    一位经验丰富的官员说,这将是一个具有战略性的影响。任何时候只要你降低性能标准,那么它的能力也会降低。
    在这个月早期时五角大楼2012年操作测试和评估主任的报告中,国防部放松原定的3个型号的肥电的消息就已经透露出来了。把空军型的稳盘过载从5.3G减到4.6G,B型从5减少到4.5G,海军型从5.1减到5G,A,B,C从0.8M到1.2M的加速时间分别延长了8秒,16秒,43秒,肥电的基本型翼尖挂2枚AIM120AMRAAMS与F16B50比较是一样的,真的让人难堪,另一个高级飞行员说,最大承受性能不到5G的肥电居然跟麦·唐的F4,诺·诺F5是一样的,它完全没有一点五代机的性能。
    一位飞行员说,站在更高的角度看,减少的性能将直接影响到飞行员面对先进的俄罗斯双数位的防空蛋蛋,比如S300PMU2时的存活力。从更低的观点看,飞行员可能在近距攻击或者争夺制空权的时候,减少的性能将使飞行员面对短程蛋蛋和防空炮火时置于更高的危险中。
    最恶劣的是C型彻底地去掉了超音速功能,飞行员说,43秒是个非常巨大的数字,后燃烧室的加速度让你非常骄傲的,即使那样会消耗更多的燃料。这会直接影响到战术执行,那不是一个好方法。
    飞行员们通常会为了2个原因中选1个做决定就是获得高燃油消耗的超音速性能,要么杀死要么保卫某个东西,在那样的情况下分秒必争,带的越多,压缩的越多,滞空时间越长。
    毫无疑问的是减少这些功能是非常错误的,可能会有方法来弥补肥电一些的比恒星运动还小的性能。
    知情人士说,飞行员有大量的肥电隐身性能和传感器补偿发动机性能,但是交战区域和操纵范围将进一步推动面对最危险的防空威胁。
    在空空状态下,比如,战术在强调隐身和视距外战斗中必须进一步发展。假如视距内交战不可避免,所有赋予肥电隐身性能的努力将被一个可能的优势地位带进漩涡中。
    一旦在视距内交战,赋予肥电的限制和相关的力量,回旋应当最小化以利于使用诺·格的AAQ37红外相机分布式系统,头盔显示器和高立轴角度导弹去攻击敌机。假如盘旋空战不可避免,肥电有良好的瞬时盘旋速度和与波音大黄蜂FA18一样的大攻击角度,意味着假如发现某人在如此的情形一个类似的战略会被采用。
    洛克希德认为肥电性能优于任何“遗留”在高海拔地区的战斗机,Steve O'Bryan说,作为一个拥有超过4000个小时的战斗机飞行员,我告诉你 肥电作为一款在高空,内部运载武器的战斗机的能力,超过任何一款我所了解的战斗机的能力,公司的业务发展总监f在1月份接受采访表示。
    但是现在大部分的讨论都是理论性的,肥电还没有完成操纵测试,也没有对于飞机战术运用方面的发展。
    飞机一旦完成开发和部署后的费用是如何的还是一个未知数。

大致翻译了一下,就是按照原文翻译的,水平有限,见谅、、、
PS,长时间不用英文,水平下降的很厉害。。。改了几个错别字

    许多具有丰富经验的战斗机飞行员被咨询时认为,五角大楼决定降低肥电的性能参数会带来重大的操作上的冲击。但是细致的战术和航空雇员的纪律可以减少这些缺点。
    一位经验丰富的官员说,这将是一个具有战略性的影响。任何时候只要你降低性能标准,那么它的能力也会降低。
    在这个月早期时五角大楼2012年操作测试和评估主任的报告中,国防部放松原定的3个型号的肥电的消息就已经透露出来了。把空军型的稳盘过载从5.3G减到4.6G,B型从5减少到4.5G,海军型从5.1减到5G,A,B,C从0.8M到1.2M的加速时间分别延长了8秒,16秒,43秒,肥电的基本型翼尖挂2枚AIM120AMRAAMS与F16B50比较是一样的,真的让人难堪,另一个高级飞行员说,最大承受性能不到5G的肥电居然跟麦·唐的F4,诺·诺F5是一样的,它完全没有一点五代机的性能。
    一位飞行员说,站在更高的角度看,减少的性能将直接影响到飞行员面对先进的俄罗斯双数位的防空蛋蛋,比如S300PMU2时的存活力。从更低的观点看,飞行员可能在近距攻击或者争夺制空权的时候,减少的性能将使飞行员面对短程蛋蛋和防空炮火时置于更高的危险中。
    最恶劣的是C型彻底地去掉了超音速功能,飞行员说,43秒是个非常巨大的数字,后燃烧室的加速度让你非常骄傲的,即使那样会消耗更多的燃料。这会直接影响到战术执行,那不是一个好方法。
    飞行员们通常会为了2个原因中选1个做决定就是获得高燃油消耗的超音速性能,要么杀死要么保卫某个东西,在那样的情况下分秒必争,带的越多,压缩的越多,滞空时间越长。
    毫无疑问的是减少这些功能是非常错误的,可能会有方法来弥补肥电一些的比恒星运动还小的性能。
    知情人士说,飞行员有大量的肥电隐身性能和传感器补偿发动机性能,但是交战区域和操纵范围将进一步推动面对最危险的防空威胁。
    在空空状态下,比如,战术在强调隐身和视距外战斗中必须进一步发展。假如视距内交战不可避免,所有赋予肥电隐身性能的努力将被一个可能的优势地位带进漩涡中。
    一旦在视距内交战,赋予肥电的限制和相关的力量,回旋应当最小化以利于使用诺·格的AAQ37红外相机分布式系统,头盔显示器和高立轴角度导弹去攻击敌机。假如盘旋空战不可避免,肥电有良好的瞬时盘旋速度和与波音大黄蜂FA18一样的大攻击角度,意味着假如发现某人在如此的情形一个类似的战略会被采用。
    洛克希德认为肥电性能优于任何“遗留”在高海拔地区的战斗机,Steve O'Bryan说,作为一个拥有超过4000个小时的战斗机飞行员,我告诉你 肥电作为一款在高空,内部运载武器的战斗机的能力,超过任何一款我所了解的战斗机的能力,公司的业务发展总监f在1月份接受采访表示。
    但是现在大部分的讨论都是理论性的,肥电还没有完成操纵测试,也没有对于飞机战术运用方面的发展。
    飞机一旦完成开发和部署后的费用是如何的还是一个未知数。
谢谢美女发新闻,你的消息渠道很广嘛
想打倒美国佬的肥电,先把美国佬的空战体系给破了,不然垃圾飞机一样致命。至于其他买肥电的倒霉鬼……自求多福吧……
vivianyoyo2002 发表于 2013-1-31 11:47
韩文的日文的我翻译了,英文应该不需要吧。。
军坛还有美女的吗
pocp 发表于 2013-1-31 19:23
大致翻译了一下,就是按照原文翻译的,水平有限,见谅、、、
PS,长时间不用英文,水平下降的很厉害。。。 ...
“空军型的从5.3G减到4.6G,B型从5减烧到4.5G,海军型从5.1减到5G”

这个说的是稳盘过载,sustained turn performance。也就是说现在35A的稳盘最大过载是4.6G
“空军型的从5.3G减到4.6G,B型从5减烧到4.5G,海军型从5.1减到5G”   这个说的是稳盘过载,sustained t ...
有没有稳盘超过7G的飞机


我来给大家翻译一下重点部分。

五角大楼在2012年的测试评估报告里决定放宽对F35的稳盘性能要求。35A的稳盘过载从5.3g下降到4.6g,35B则是5g减到4.5G,35C从5.1G减到5G。从0.8马赫到1.2马赫的加速时间,F35A延长了8秒,35B是延长了16秒,35C是延长了43秒!有经验的飞行员评论到稳盘过载下降到了少于5g,这已经是等于F4或F5的水准了。

更臭名昭著的是35C那严重恶化的超音速加速性。43秒的时间太长了,而且这个开加力的加速过程会消耗更多燃油。

性能不足战术补,有经验的美国飞行员建议35尽量采用BVR,避免狗斗。当狗斗不可避免,则主要靠瞬盘和大迎角性能。35的大迎角性能和F18相似。另外狗斗还得靠分布式孔径光电系统和大离轴角导弹、头盔显示器。总之这些都是老生常谈了

这篇新闻最大的意义是明确了现在的35系列稳盘过载指标和超音速加速时间

我来给大家翻译一下重点部分。

五角大楼在2012年的测试评估报告里决定放宽对F35的稳盘性能要求。35A的稳盘过载从5.3g下降到4.6g,35B则是5g减到4.5G,35C从5.1G减到5G。从0.8马赫到1.2马赫的加速时间,F35A延长了8秒,35B是延长了16秒,35C是延长了43秒!有经验的飞行员评论到稳盘过载下降到了少于5g,这已经是等于F4或F5的水准了。

更臭名昭著的是35C那严重恶化的超音速加速性。43秒的时间太长了,而且这个开加力的加速过程会消耗更多燃油。

性能不足战术补,有经验的美国飞行员建议35尽量采用BVR,避免狗斗。当狗斗不可避免,则主要靠瞬盘和大迎角性能。35的大迎角性能和F18相似。另外狗斗还得靠分布式孔径光电系统和大离轴角导弹、头盔显示器。总之这些都是老生常谈了

这篇新闻最大的意义是明确了现在的35系列稳盘过载指标和超音速加速时间
唉'一声叹息'我的肥电啊
蛤蟆值夜班 发表于 2013-1-31 20:30
有没有稳盘超过7G的飞机
稳盘超过7g的有没有我不清楚 没有看过太多这方面资料,从常识推断不太可能,因为要超过人类耐受极限了。

但这篇新闻里,美国的资深飞行员说,稳盘小于5g是F4、F5的水平。
美帝有F22 不怕 可惜 像英国和日本就被坑了啊。。
F35降低指标又给晨风之流送炮弹啦
对美帝没啥影响,但对于把肥电当空优战机的国家来说是个不好的消息
怕个啥。实在不行都都塞给脚盆,让它们去负担成本就是了
mygodson 发表于 2013-1-31 19:11
35的背部不错,腹部真心不好看
没有肌肉虬结的力量感?
neverdavis 发表于 2013-1-31 20:39
稳盘超过7g的有没有我不清楚 没有看过太多这方面资料,从常识推断不太可能,因为要超过人类耐受极限了。
...

上面是瞬盘范围
下面是稳盘范围

可以看到F-16在一定的速度和高度时可以做到稳盘9G
pocp 发表于 2013-1-31 19:23
大致翻译了一下,就是按照原文翻译的,水平有限,见谅、、、
PS,长时间不用英文,水平下降的很厉害。。。 ...
多谢翻译~~估计我翻的话,还不如你呢,好多专门的词我都没听过。。。:L
neverdavis 发表于 2013-1-31 20:15
谢谢美女发新闻,你的消息渠道很广嘛
嘿嘿,我这种打酱油的就只能在这方面给CD做点贡献了。。:D
chan4461 发表于 2013-1-31 20:18
军坛还有美女的吗
性别女没错,美还是不美这事儿我说的不算,得别人评判 哇咔咔卡
neverdavis 发表于 2013-1-31 20:37
我来给大家翻译一下重点部分。

五角大楼在2012年的测试评估报告里决定放宽对F35的稳盘性能要求。35A的稳 ...
学习了。。。看了中文也不明白再讲什么。。。唉~~
pocp 发表于 2013-1-31 19:23
大致翻译了一下,就是按照原文翻译的,水平有限,见谅、、、
PS,长时间不用英文,水平下降的很厉害。。。 ...
clean是说无多余挂载的意思,后面也说了,只有两枚翼尖格斗弹
只用8秒是不可能从0.8加速到1.2马赫的,即使在真空中不考虑空气阻力也不行,计算如下
330m/s * 0.4 / 8s = 16.5m/s2 这是加速度
根据 F=Ma 可知 F=16000kg * 16.5m/s2= 264000牛 就是264千牛,远大于F-135发动机推力
况且这没算空气阻力,就是说在真空里也不行

所以所谓0.8-1.2马赫加速用时8秒,只可能是增加了8秒而不可能是增加到8秒
这翻译惨不忍睹啊。

俺就说下标题,不是影响操作,而是影响作战。正文里直接说了,美军的老鸟们都认为会对"战术"产生重大影响。
vivianyoyo2002 发表于 2013-1-31 21:57
多谢翻译~~估计我翻的话,还不如你呢,好多专门的词我都没听过。。。
俺会告诉你我用了词典吗{:qiliang:}
汉军 发表于 2013-2-1 07:40
这翻译惨不忍睹啊。

俺就说下标题,不是影响操作,而是影响作战。正文里直接说了,美军的老鸟们都认为会 ...
用“运作”更贴切一点吧?至少保留了“operational”的愿意~~
没写多大速度下的指标降低啊。 15000m,4g M1.8的话,即便降低了依然很强啊。
用“运作”更贴切一点吧?至少保留了“operational”的愿意~~
兄弟,IOC,Initial operating capability,初始作战能力,听说过吧?运作也不是不可以,但战斗机的运作,不就是作战吗?通篇讲的不就是对战术的悲剧性影响吗?
我来给大家翻译一下重点部分。

五角大楼在2012年的测试评估报告里决定放宽对F35的稳盘性能要求。35A的稳 ...
兄弟,再看下原文,加速性能是"增加了",还是"增加到"?
behappy99 发表于 2013-2-1 06:28
只用8秒是不可能从0.8加速到1.2马赫的,即使在真空中不考虑空气阻力也不行,计算如下
330m/s * 0.4 / 8s = ...
是增加了8秒,我翻译时候错了 已改
汉军 发表于 2013-2-1 11:45
兄弟,再看下原文,加速性能是"增加了",还是"增加到"?
嗯 多谢指正,extended by,确实应该是增加了而不是增加到,已改。
汉军 发表于 2013-2-1 11:36
兄弟,IOC,Initial operating capability,初始作战能力,听说过吧?运作也不是不可以,但战斗机的运作, ...
坦白说, 没听过IOC。。。那还是改成作战吧!thanks!
减少F-35的性能指标有显着的运行产生影响

戴夫·马宗达华盛顿DC:


五角大楼的决定,以减少洛克希德·马丁公司的F-35联合攻击战斗机的性能规格,将有一个显着的运行产生影响,一些经验丰富的战斗机飞行员咨询Flightglobal同意。但细心的发展策略和纪律就业的喷气也许能够减轻一些这些缺点。

“这将有一个大的战术的影响,”一个经验丰富的军官说。 “只要你有降低性能标准,机身可以做什么的能力”以及“。



美国国防部的决定放宽三个变种F-35的持续转弯性能,本月早些时候透露,在五角大楼作战测试和评估2012报告主任。从5.3持续的克氏4.6持续克,将美国空军的F-35A的性能降低。从5到4.5克的F-35B持续克的切割,而美国海军的变体有它的转弯性能从5.1截断持续到5克的。为A,B和C模型分别从0.8马赫到1.2马赫的加速时间分别延长了8秒,16秒和43秒。用于比较的基线标准是一个干净的洛克希德F-16有两个翼尖雷声公司的AIM-120 AMRAAMs 50座。 “好尴尬,会有明显的战术意义。小于5g,最大持续转弯性能是相当于[麦道公司的F-4或[诺斯罗普F-5,”另一个经验丰富的战斗机飞行员他说。 “[这是]当然没有任何接近的第四和第五代战机的性能。”

海拔越高,性能降低,将直接影响对先进的俄罗斯设计的“两位数”表面对空导弹(SAM)系统,如阿尔马兹-Antey S-300PMU2(也被称为SA-20石像鬼的生存能力北大西洋公约组织),飞行员说。在低海拔地区,其中战斗机可能在运作中的近距离空中支援,或前进空中控制作用,减少机体的性能将飞行员对短程地空导弹和高炮的风险增加。

最令人震惊的是F-35C模型的大幅降低跨音速加速功能。 “[43秒]是一个大量的时间,并假设你是在加力加速,它会花费你更多的气体,”飞行员说。 “这将直接影响到战术执行力,而不是在一个很好的方式。”

飞行员作出决定交易的燃油消耗率非常高超音速空速为以下两个原因之一。 “他们是准备去刷怪,或者他们正试图抵御的东西试图杀死他们,”飞行员说。 “每分每秒,这些方案的时间越长,越压缩的战斗空间得到,这是不是一件好事。”



虽然是没有争议的,降低性能指标是一个负面的发展,有很多方法可以弥补一些F-35的小于恒星运动性能。

飞行员必须使F-35的隐身特性和传感器的广泛使用,以弥补的喷射性能方面有弱点,与飞机的知情人士说。但是参与区域和机动范围将最有可能被驱动,甚至更远对最危险表面的空中威胁。

在空气 - 空气接触,例如,战术必须强调隐身性和超视距(BVR)作战。如果一个视觉范围内的参与是不可避免的,将尽一切努力,必须采取进入“合并”的位置优势,这应该是可能的,F-35的隐身特性。

一旦从事可视范围内,给出了F-35的局限性和相对优势,转弯应该被最小化有利于使用在飞机的诺斯罗普·格鲁门公司AAQ-37分布式孔径系统的红外摄像机,头盔,安装显示屏和高离轴发射导弹搞敌人的飞机。如果一个转折点的战斗是不可避免的,F-35具有良好的的瞬时转弯性能和良好的高攻角(50°攻角限制)性能相媲美的波音F/A-18“大黄蜂”,这意味着一个类似的策略可以采用,如果一个发现他或她自己在这样的情况下。


它的一部分,洛克希德,坚持认为F-35性能优越的“遗产”战机在高海拔地区的任何。 “在飞行超过4000小时的战斗机,我会告诉你的F-35的能力,在高海拔地区,大部分驱动的内部运送这些武器,作为一个作战飞机,这架飞机超过的只是任何旧的战斗机,我'的能力米熟悉这种制度,O'Bryan,该公司的业务发展总监的F-35在一月份的采访中说:“史蒂夫。

不过多的讨论是理论,在这一点上,F-35还没有被运行测试,也没有战术飞机的使用。飞机最终将票价一次充分的开发和部署的是一个悬而未决的问题