Infra_Man99
Banned Idiot
Regarding the Jane's article on the F-35 JSF, I don't think the JSF is anywhere that bad. I actually think the JSF will be a good fighter/attack jet. Here's my rebuttal of the above Jane's article:
1. The assumed information by Jane's about the JSF may be false. The US military does send out disinformation. Look how well the US military sold the very questionable Iraq War and how the US military is hiding what is completely going on in Iraq and Afghanistan.
2. The JSF may not be overweight. It can hold a maximum of ~18,000 lb of internal fuel (it depends on the JSF's 3 models: A, B, and C). The F-16 holds a maximum of ~7,000 lb of internal fuel and the F-16 flies most missions with external fuel tanks and external fuel tanks adds weight, drag, and wear-and-tear on the wings. In other words, the JSF may be overweight, but mostly because it can hold an enormous amount of internal fuel. Once the JSF flies into its combat zone, it could only have 2/3rd of its fuel left.
(2/3) X (18,000 lb of max internal fuel) = 12,000 lb still in the internal fuel tanks by the time the JSF reaches its combat zone.
18,000 lb -- 12,000 lb = 6,000 lb used up in the internal fuel tanks by the time the JSF reaches its combat zone.
So the JSF could have lost 6,000 lb by the time it reaches its combat zone. This will improve the JSF's thrust-to-weight ration and wing loading. The same thing applies to all combat planes.
3. In realistic situations, the JSF has at least comparable performance to the F-16. Check out the data.
JSF vs. F-16
Empty Weight: ~29,000 lb to ~32,000 lb (depends on the model A, B, or C) vs. ~19,000 lb
Fuel Capacity: ~18,000 lb internally vs. ~18,000 lb internally and externally
Configuration 1 = Empty Weight + ~18,000 lb of fuel + 1,200 lb of 4 missiles: 48,200 lb to 51,200 vs. 32,000
Dry Thrust: 25,000 lb vs. 17,155 lb
Dry Thrust to Weight Ratio (w/ configuration 1): 0.51 to 0.488 vs. 0.536
Max Thrust: 40,000 lb vs. 28,600 lb
Max Thrust to Weight Ratio (w/ configuration 1): 0.83 to 0.78 vs. 0.89
Wing Area: 459.6 sq ft vs. 300 sq ft
Wing Loading (w/ configuration 1): 104.87 lb per sq ft to 111.4 lb per sq ft vs. 106.67 lb per sq ft.
Remember that the JSF does all of this with a clean configuration (everything is carried internally) but a similarly equipped F-16 will need external fuel tanks and the F-16 carries all missiles (and bombs) externally under its wings. This means a combat ready JSF is probably much more aerodynamic than a combat ready F-16 or any other combat-ready, 4th-gen fighter jet. This means the combat ready JSF could be more fuel efficient, faster, more agile, have no increased radar signature, and experience less wear-and-tear on its wings and weapons when compared to 4th gen fighter jets.
The JSF has very advanced electronics and it could have 2-D or 3-D vectored thrust. The JSF should have more advanced air intakes than the F-16.
The result: The clean JSF COULD have superior performance in most situations than the externally loaded F-16.
4. The JSF can internally carry 4 missiles, and each AMRAAM weights less than 400 lb, so the clean JSF can carry 4 missiles without greatly lowering its thrust-to-weight ratio, wing loading, putting extra wear-and-tear on its wings, and ruining its slick aerodynamics.
5. The advanced, stealthy JSF has far superior electronics and a much smaller radar signature than the F-16. Teamwork is very important for the military, even for small units like the Navy SEALs. The JSF should have a variety of modern communication systems so it could work well with other military personnel and military tools like other fighter jets, AWACs, ground support, satellite assistance, central command, and naval ships.
The JSF is not perfect, but it seems like a good fighter jet to replace the F-16 and F/A-18. The JSF lacks the F-15 fighter jet's larger radar, top speed, high-speed acceleration (acceleration from Mach 1.0 to Mach 2.5) , and external capacities, but the JSF is much, much more stealthy, it is probably more agile, and it can fly clean, so the JSF may cruise faster (super cruise?) and more efficiently than the F-15 from Mach 0.0 to Mach 1.6. I guess that an F-15 fighter jet with its typical external weapons load is UNABLE to reach Mach 2.5. If it can, then it does so with lots of drag and wear-and-tear.
The JSF may not be an overweight, expensive 5th generation fighter jet. I think a better description of the JSF is an expensive 5th generation fighter jet with ENORMOUS internal capacities and optional, large external capacities.The JSF is a good 5th generation fighter jet when you look at its whole package.
With AWACs, then things get pretty complicated and I'll leave out AWACs even though AWACs is extremely important in modern and future air combat.
I am just a fan of military stuff. What do the more knowledgeable members think of my analysis of the JSF?
1. The assumed information by Jane's about the JSF may be false. The US military does send out disinformation. Look how well the US military sold the very questionable Iraq War and how the US military is hiding what is completely going on in Iraq and Afghanistan.
2. The JSF may not be overweight. It can hold a maximum of ~18,000 lb of internal fuel (it depends on the JSF's 3 models: A, B, and C). The F-16 holds a maximum of ~7,000 lb of internal fuel and the F-16 flies most missions with external fuel tanks and external fuel tanks adds weight, drag, and wear-and-tear on the wings. In other words, the JSF may be overweight, but mostly because it can hold an enormous amount of internal fuel. Once the JSF flies into its combat zone, it could only have 2/3rd of its fuel left.
(2/3) X (18,000 lb of max internal fuel) = 12,000 lb still in the internal fuel tanks by the time the JSF reaches its combat zone.
18,000 lb -- 12,000 lb = 6,000 lb used up in the internal fuel tanks by the time the JSF reaches its combat zone.
So the JSF could have lost 6,000 lb by the time it reaches its combat zone. This will improve the JSF's thrust-to-weight ration and wing loading. The same thing applies to all combat planes.
3. In realistic situations, the JSF has at least comparable performance to the F-16. Check out the data.
JSF vs. F-16
Empty Weight: ~29,000 lb to ~32,000 lb (depends on the model A, B, or C) vs. ~19,000 lb
Fuel Capacity: ~18,000 lb internally vs. ~18,000 lb internally and externally
Configuration 1 = Empty Weight + ~18,000 lb of fuel + 1,200 lb of 4 missiles: 48,200 lb to 51,200 vs. 32,000
Dry Thrust: 25,000 lb vs. 17,155 lb
Dry Thrust to Weight Ratio (w/ configuration 1): 0.51 to 0.488 vs. 0.536
Max Thrust: 40,000 lb vs. 28,600 lb
Max Thrust to Weight Ratio (w/ configuration 1): 0.83 to 0.78 vs. 0.89
Wing Area: 459.6 sq ft vs. 300 sq ft
Wing Loading (w/ configuration 1): 104.87 lb per sq ft to 111.4 lb per sq ft vs. 106.67 lb per sq ft.
Remember that the JSF does all of this with a clean configuration (everything is carried internally) but a similarly equipped F-16 will need external fuel tanks and the F-16 carries all missiles (and bombs) externally under its wings. This means a combat ready JSF is probably much more aerodynamic than a combat ready F-16 or any other combat-ready, 4th-gen fighter jet. This means the combat ready JSF could be more fuel efficient, faster, more agile, have no increased radar signature, and experience less wear-and-tear on its wings and weapons when compared to 4th gen fighter jets.
The JSF has very advanced electronics and it could have 2-D or 3-D vectored thrust. The JSF should have more advanced air intakes than the F-16.
The result: The clean JSF COULD have superior performance in most situations than the externally loaded F-16.
4. The JSF can internally carry 4 missiles, and each AMRAAM weights less than 400 lb, so the clean JSF can carry 4 missiles without greatly lowering its thrust-to-weight ratio, wing loading, putting extra wear-and-tear on its wings, and ruining its slick aerodynamics.
5. The advanced, stealthy JSF has far superior electronics and a much smaller radar signature than the F-16. Teamwork is very important for the military, even for small units like the Navy SEALs. The JSF should have a variety of modern communication systems so it could work well with other military personnel and military tools like other fighter jets, AWACs, ground support, satellite assistance, central command, and naval ships.
The JSF is not perfect, but it seems like a good fighter jet to replace the F-16 and F/A-18. The JSF lacks the F-15 fighter jet's larger radar, top speed, high-speed acceleration (acceleration from Mach 1.0 to Mach 2.5) , and external capacities, but the JSF is much, much more stealthy, it is probably more agile, and it can fly clean, so the JSF may cruise faster (super cruise?) and more efficiently than the F-15 from Mach 0.0 to Mach 1.6. I guess that an F-15 fighter jet with its typical external weapons load is UNABLE to reach Mach 2.5. If it can, then it does so with lots of drag and wear-and-tear.
The JSF may not be an overweight, expensive 5th generation fighter jet. I think a better description of the JSF is an expensive 5th generation fighter jet with ENORMOUS internal capacities and optional, large external capacities.The JSF is a good 5th generation fighter jet when you look at its whole package.
With AWACs, then things get pretty complicated and I'll leave out AWACs even though AWACs is extremely important in modern and future air combat.
I am just a fan of military stuff. What do the more knowledgeable members think of my analysis of the JSF?
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