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wrightwing

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  • in reply to: F-35 Debate thread (2) #2278031
    wrightwing
    Participant

    The F35 costs how much for a far from operational, non-effective platform that clearly has limited opportunity for any degree of enhancement once actually in service?

    See the difference?

    Hmmmm, Block 4, 5, 6, 7…..

    in reply to: What if JSF was split into two separate programmes? #2240633
    wrightwing
    Participant

    F-35C can’t land on carriers there for has a 7.1 hook distance.But Lockmart can fix this issue
    http://3.bp.blogspot.com/-VqEq1NKQMTc/TwagY9J7qTI/AAAAAAAAByQ/OW26Nwx3-9U/s1600/hooklocationC.png

    USAF and USN F-35’s are mostly a “Jack Of All Trades” master of none. The F-35 may not be a good air superiority fighter as how the F/A-18 and F-16 performed, it may not be the CAS platform the A-10 was. But the F-35 is serving as the better “Bomb Truck” with perfect bomb payload and range. Great avionics and situational awareness in Ground Attack.
    But it’s serving well with the AV-8B replacement which is a master of a trade.

    I agree it has lower speed, acceleration and T/W Ratio. But the USN version is worse with the lower T/W Ratio.

    USN F-35 T/W Ratio
    With 50% of fuel = 0.91
    with full fuel is 0.75

    USMC T/W Ratio
    Full Fuel=0.90
    50%f uel=1.04

    USAF T/W Ratio
    Full Fuel=0.87
    50% Fuel=1.07

    As you see it may not be the best air-to-air performer out there but still capable in BVR. In WVR, we’ll leave it up to the real pilots who fly it, or when deployed in a exercise. But although the F-35 is a great bomb truck.

    It’s a great bomb truck, and superior to the F-16/18 in A2A as well. As for the F-35C can’t land on carriers, you may want to look at more recent results.

    in reply to: What if JSF was split into two separate programmes? #2241308
    wrightwing
    Participant

    Well the F-35A can’t operate from carriers, so this plan would entail both the USAF and USN using the the C model, resulting in the USAF getting less airframes (higher cost), and lower overall performance. (slower acceleration/G loading) Unless the USMC went with an aircraft much more akin to the AV-8B, there’d hardly be any cost savings realized.

    wrightwing
    Participant

    Since when does NATO have a problem with China?

    They can. The more important question is why would they want to? They would then have to develop another network, to allow full functionality, instead of something that already works. Seems to be a rather inefficient allocation of resources.

    in reply to: F-35 Debate thread (2) #2245169
    wrightwing
    Participant

    No sources = no arguments. Just your own speculation without any proof…

    Let’s just call it an educated guess. I started with a number that several here are taking as Gospel, of 20nm for the AIM-120C5. I then took a conservative range of percentages of improvement, that the C7/D have been attributed with, along with the kinematic advantages that the F-22 bestows, from firing at high speed/altitude. The assumptions are all high altitude shots, against a head on target. Obviously at low altitude, tail chase, etc…., the ranges will be significantly lower.

    in reply to: F-35 Debate thread (2) #2245858
    wrightwing
    Participant

    Thats where i am coming from as well. As pure physics is concerned, it is true that the best maneuverability would be with the motor thrusting, but the missile requirements require it to be able to execute performance after burn out and to overcome significant threats with agility and sensors. The NEZ of a modern BVR missile goes much beyond the simple burn out distance and this can be confirmed by just talking to most fighter pilots. The meteor , Aim-120, R-77, Mica’s of this world can kill a maneuvering fighter well beyond burn out. Modern 4.5 – 5th gen fighters can also passively cue their BVR weapons towards their targets without the missile having to go active and alert the RWR’s as well….The actual performance is of course classified, but the air forces of the world both in the west and russia/china are increasing their investments in BVR both as a means of engaging the enemy in it as well as defending against it…so it is fairly logical to conclude that the True BVR combat possible with modern missiles and fighters is well beyond the NEZ of 15 km – 20km being sited here…

    Exactly. Missiles make up for turn radii, with sheer speed.

    in reply to: F-35 Debate thread (2) #2246003
    wrightwing
    Participant

    2. F-22A has probably the best kinematics of all current fighters. It can shoot AMRAAM from 1,7 Mach + 40k ft+, which give the missile a lot of range compared to the others fighter. Very important thing is acceleration from 0,9 mach ( even raptor fly economically before detect targets) to Mach 1, + so you need to gain energy when you are ~ 100-200km from target (EW, reduced RCS, low flying target, passive detection, etc make detection more difficult ).
    3. 20 miles is actual effective AIM-120C-5/7 AMRAAM range when fired from Raptor – we all know that Raptor fire AMRAAM and then turn away, thx to link 16 other F-22 guys can guide missile by radar/ALR-94 combo.
    4. We all know that F-15C shoot AMRAAM from 25 km (35k ft+ 1,4 Mach) in real war games… against poor equiped MiGs.
    So I don’t understand why some guys here can’t accept the facts #3 because:
    -AIM-120C has 10% better range than AIM-120B

    -Assuming that we go with the AIM-120C5 having a 10% range improvement over the B. That still doesn’t account for the C7, which has a ~10 to 30% improvement over the C5. Now when fired from the F-22 at high speed/altitude, you can add another 30-50% to the range. So, just doing some basic beer math-
    C5= ~20nm
    C7= ~22-26nm
    C5 fired from F-22 (supercruise/high altitude/head on)= ~26-30nm
    C7 fired from F-22 (supercruise/high altitude/head on)= ~28.6-45nm
    D= ~33-39nm
    D fired from F-22= ~49.5nm-58.5nm

    Now if we don’t assume that the C5 is limited to 20nm fired (from high altitude in a frontal engagement,) and is in fact higher, then the other corresponding range figures increase as well.

    If we assume a 30nm range, then then numbers start to look like-
    C5= ~30nm
    C7= ~33-39nm
    C5 fired from F-22= ~39-45nm
    C7 fired from F-22= ~42.9-58.5nm
    and just for fun
    D= ~49.5-58.5nm
    D fired from an F-22= ~64.35-87.75nm

    in reply to: F-35 Debate thread (2) #2248652
    wrightwing
    Participant

    From what i gather, F-35 will spend about all its missions at 20-30k ft,
    isnt that what is advocated as an advantage of F-35 anyway ?
    not ever having to fly low, but on the contrary the higher away from ground radar the better ?

    I imagine the profile will be dependent on the mission. If you need more range, then more efficient altitudes will be chosen. If flying an A2A mission, then the F-35 will most likely be flying in the 35-45k ft altitude range (or higher). It will also be lighter carrying only AAMs.

    in reply to: F-35 Debate thread (2) #2248654
    wrightwing
    Participant

    initially, it’s from Lockheed presentation to Norway if my memory serves well… looks like quite a small gain, but that may illustrate the drag increase (and therefore, the increase in fuel consumption) with external stores. The extra tanks may be interesting not to increase the overall range, but to maintain range when stuff is hanging outside…

    What I’d like to know is if the first range figure was for internal carriage only, and the second range figure was for tanks, and external stores. If so, then that would make sense.

    in reply to: F-35 Debate thread (2) #2249429
    wrightwing
    Participant

    It doesn’t make sense that 2 tanks of fuel, would only get you another 56nm. One of those figures has to be off.

    in reply to: F-35 Debate thread (2) #2249938
    wrightwing
    Participant

    [QUOTE=Andraxxus;2036224]No, math is very accurate, but comparison logic is slightly flawed:

    An F-16 with only 370 gal tanks have 688 nm combat radius.[quote]
    What use is an unarmed F-16, flying with 2 370 gal tanks?

    F-35’s undisclosed combat radius is 590 nm with full internal fuel load of 18500 lb.

    Actually that’s not accurate. That figure was based upon an arbitrary reserve amount, during the testing process, and without giving the specifics of the mission profile, time on station, afterburner usage over target area, etc..

    For F-35, to reach 814 nm combat radius, it needs fuel tanks; How many? Assuming “miles per pound” stays same -which is not possible due to increased drag and weight-, it will need at least ~7030 lb of fuel, which equals to 1064 gallons.

    There’s no mission where an F-16 has an 814nm combat radius, without aerial refueling.

    in reply to: F-35 Debate thread (2) #2250876
    wrightwing
    Participant

    And I say it failed in this regard. Judging by the info at hand, it barely matches/exceeds F-16’s kinematic performance in some areas, and not even approaching in others. I am not saying F-35 is inferior to F-16 as overall package, and I am aware of the leap of capability it has made. I am saying its kinematics will be inferior to F-16 for 80% of the time, and inferior to F-15 it replaces 99% of the time.

    In real world conditions, I think that you have your numbers reversed, in terms of kinematic advantages.

    in reply to: F-35 Debate thread (2) #2251706
    wrightwing
    Participant

    When has this occurred first of all. Secondly assuming that such a feat was possible, it wouldn’t be of much use in combat, as an F-16 without EFTs, isn’t going to have particularly impressive range as is (much less in full AB). Additionally, with EFTs and sensor/jamming pods, it’d never get close to that speed. The fastest that an F-15 in A/A load out, has flown in real world conditions, was ~M1.4.

    in reply to: F-35 Debate thread (2) #2252353
    wrightwing
    Participant

    Have you got any credible sources for this?
    According to RAF AIM-120C-5 has 10% better operational range than C-5 (2012 Air International , Typhoon A Year on the road). And yes -Raytheon gives 50% greater range to C-5, 30% better range for C-7, and another 50% better range for future D-model, this value could be true for balistic range of missile, and according to RAF pilots the usefull range is much smaller ( 50% vs 10% increasement in B vs C AMRAAM model comparsion ). Choose what you believe. I give you a solid sources for this.

    A source, to be more precise. I’m not going to get into a debate over anecdotes. We don’t know what conditions that the RAF were referring to when making that statement, versus the conditions the USAF or Raytheon, might be using for different range statements, and without that we can’t do an apples to apples comparison.

    in reply to: F-35 Debate thread (2) #2252379
    wrightwing
    Participant

    The PR department claim F-35 flies better than anything else for as long as it has any combat load.
    Incorrect as far as A2A loadout goes, but correct if combat load=2×2000 lbs bombs

    Well, if it’s being compared to F-16/18s (or 4th Gen fighters in general), even in an A/A configuration, they’d have EFTs, and the F-35 would be even lighter in A/A configuration (handle better, than in A/G).

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