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  • in reply to: test pilot: "F-35 can't dogfight" #2157283
    mig-31bm
    Participant

    Thx for posting the whole article.
    Now try your very best to spin this your way 😉

    Sergei Bogdan himself say he accelerated to mach 1.1

    By how much is the airfoil ticker?
    All other features points towards S-35S
    Angle of sweept back wings, also air-intakes, cockpit design
    long pointy nose that gives less skin friction drag.
    Longer airframe has better drag feature vs a short stubby one.
    .

    i dont think the Su-35 have better cockpit , Su-35 is longer but it is also alot bigger meaning more skin drag
    i do agree that the intake of Su-35 is better for supersonic , but then again i also heard fixed intake can provide pressure recovery well until mach 1.3
    Su-35 wing seem sweep back more than F-35 , but then it is thicker , So iam not sure how much their drag compare to the other (and i know you dont either )
    May be Andraxxus can help with some calculation

    in reply to: Eurofighter Typhoon discussion and news 2015 #2157291
    mig-31bm
    Participant

    What is that hole in Typhoon vertical tail for
    http://www.globalaviationresource.com/v2/wp-content/gallery/coningsby-gripens/IMG_8543.jpg

    in reply to: test pilot: "F-35 can't dogfight" #2157298
    mig-31bm
    Participant

    According to Sergey Bogdan’s, the Su-35S accellerated up to Mach 1.3 on mil power at medium altitude.
    And it was still accellerating while he disengaged and turned back to base.

    .

    On Mil power he only accelerated to mach 1.1
    The mach 1.3 at 11000 meters is about part of the flight testing rather than about supercruise

    During the test flight at the highest thrust regime without the use of afterburner the Su-35 achieved Mach 1.1 speed and was still accelerating
    By late June, the no. 1 flying prototype had completed 13 test missions. These were devoted to assessment of the airplane’s stability and controllability, maneuvering characteristics and powerplant performance. In addition, the operation of onboard systems was closely monitored. Having received a generally positive assessment of the aircraft, Sukhoi sent it into the supersonic regime. On mission 12, the airplane accelerated to Mach 1.2 at medium altitudes (up to 6,000 meters). The next flight went as high as 11,000 meters and reached speeds of Mach 1.3.
    Importantly, the airplane demonstrated its ability to maintain supersonic speed at military power (the highest thrust regime without the use of afterburner). Sergei Bogdan selected his words carefully, but did state: “At medium altitudes and with military power, the airplane was making a moderate supersonic speed and still accelerating. In one of the flights, I achieved Mach 1.1, and while the aircraft could accelerate further, I had to slow down because I was approaching the end of our supersonic flight zone.”

    You have heard this many times by now and it is very plausible.
    The 117S has 8.800kgf on dry mil power. That is 17.500kgf of dry thust on a fighter design which is vastly aerodynamic superior over F-35.

    i agree that it is plausible that Su-35 can fly supersonic without afterburner , but so is F-35 according to pilot statement , neither of them can supercruise in the same way as F-22 or Typhoon
    and while Su-35 have higher total thrust , it is also alot bigger than F-35 and have thicker wing

    in reply to: test pilot: "F-35 can't dogfight" #2157300
    mig-31bm
    Participant

    I’ve been around here for a long Time.
    Don’t act like you don’t know the early LockMart SC stamp.

    Yes it started with F-22.
    Then F-35 started off as SC requirement very early in its development.
    Guess LM thought the Huge F135 was a savoir, and SC was a fact.

    Later in F-35 development, it quickly became clear that this was doubtfull.
    Then the first report of F-35 KPP came out.
    The SC requirement from LM vanished like smoke on the water from their advs divisjon.

    Supercruise was never a requirement for F-35
    If F135 was designed for supercruise , it would have been similar to F119 engine , The increased BPR eliminates the “super cruise” performance of the F119 as it was not a requirement of the JSF (F-35 Lightening) program

    The F-35 can’t do Mach 1.2 in SC.
    End of story.

    according to pilot it can maintain mach 1.2 without afterburner for 150 miles

    By SC deffinition.
    The F-15E, EF and Su-35S can.

    an F-15E without CFT , EFT , carry only AAM can fly at mach 1.08 without afterburner
    There is 1 forum source stated that a clean Su-35 can fly past mach 1.1 on dry thrust , Sukhoi themselves doesnt claim Su-35 can supercruise with AAM either
    No one ever deny that EF-2000 can supercruise so i dont know why you bring it up

    in reply to: test pilot: "F-35 can't dogfight" #2157373
    mig-31bm
    Participant

    His data (referring to post at f-16.net) is wrong, here is the chart:
    [ATTACH=CONFIG]241777[/ATTACH]

    So F-15E can supercruise @ M1,14 only when clean. As for F-15E drag index system, its 4 pages long but to name few relevant items;
    LAU-128A launcher + ADU-552A adapter (used for both AIM-120 and AIM-9) -> Drag index = 1,1
    AIM-120A -> 2,3 on wing stations, 1,3 if mounted conformally, 1,7 if mounted on CFT stations. (note that conformal mounting does not require launcher/adapter)
    AIM-9M -> 2,1
    Type 4 CFT -> 20,1
    Type 5 CFT -> 21,3
    LANTIRN -> 9,5 + 7,4 if carrying cft mounted A-G stores, 7,4 + 6,5 if not.
    Mk-82 -> 0,8 if mounted without bombs/tanks on wing stations, 0,9 if mounted with bombs/tanks on wing stations
    GBU-12 -> 3,9 if mounted without bombs/tanks on wing stations, 4,3 if mounted with bombs/tanks on wing stations
    Mk-84 -> 3,0 if mounted on centerline, 2,1 if mounted on wing without cft, 2,3 if mounted on wings with cft, 2,8 if mounted on cft stations without bombs/tanks on wings, 3,0 if mounted on cft stations with bombs/tanks on wings.
    GBU-10 -> 10,5 if mounted on centerline, 7,5 if mounted on wings, 9,8 if mounted on cft stations without bombs/tanks on wings, 10,7 if mounted on cft stations with bombs/tanks on wings.
    610 Gal Fuel tank -> 12,2 if mounted on centerline, 5,5 if mounted on wing without cft, 6,0 if mounted on wings with cft, 12,3 if mounted on wings with cft with bombs on outboard cft station.

    So with CFT and minimalist armament of 4 AIM-120s, F-15E can barely exceed mach 1. Without CFT, it can supercruise slightly faster than M1,08 with 8x AIM-120s, or 4xAIM-120s+4xAIM-9s, or LANTIRN + 2xMk-84 bombs, or 4xAIM-120s + 2x Wing fuel tanks.

    I think he mentioned the F-15 that can supercruise at mach 1.14 when carry 50% fuel no tanks/CFT 4xAIM-7 2XAIM-9 is the one equipped with F110-GE-129 , may be it is different from F-15 with F100PW229 ?

    in reply to: test pilot: "F-35 can't dogfight" #2157377
    mig-31bm
    Participant

    I do not disgree.
    But there was at first the SC F-35.
    Then there was the F-35, relaxed SC.
    And what you state now, the F-35 not SC.

    LockMart at its best..

    Its debateble if SC Mach 1.2 with weapons is useful or not..
    It least You’re get better accellerating performance up the charts, which could mean less time on AB.

    Ok , according to official statement ” F-35 can maintain 150 miles without using afterburner ” the problem is we dont know exactly why it is only 150 miles , it could be that F-35 need to use afterburner to pass the mach barrier and stayed for 150 miles at mach 1.2 before decelerated bellow that , it could be that 150 miles is part of total combat radius ( similar to how they put stated F-22 combat radius included only 100 nm supercruise )…etc.
    If you consider what F-15E , Su-35 and Mig-31 did is supercruise then F-35 can supercruise
    IF you only consider aircraft that can go at mach 1.4-1.5 in dry thrust with external weapon then obviously none of these aircraft mentioned above can supercruise

    in reply to: test pilot: "F-35 can't dogfight" #2157511
    mig-31bm
    Participant

    Ofcourse you have heard it before.
    You just keep ignore it.

    .

    No haavarla
    I havent seen official source that claim Su-35 or F-15 can supercruise with weapon
    searching on Google the closest result is this :

    During the test flight at the highest thrust regime without the use of afterburner the Su-35 achieved Mach 1.1 speed and was still accelerating
    ……
    Sukhoi continues assessments of the recorded parameters in order to determine whether the airplane had actually attained supercruise.
    Additionally, the company continues to define altitudes, weights, external and internal loads at which the Su-35 can reach its supercruise performance.

    http://forum.keypublishing.com/showthread.php?85695-Thrust-Vector-Controls-in-Su-30-35

    With this configuration
    100% trim MIL power
    50% fuel no tanks/CFT
    4xAIM-7
    2XAIM-9

    ICAO standard day at 31000-36000feet

    F-15E with F100-PW-220 M1.03
    F-15E with F100-PW-229 M1.08
    F-15E with F110-GE-129 M1.14

    How do I know? I have the flight manual in front of me and the graphs of the USAF test with -129s in the E model. Tomorrow I’ll get out the C model books and get their cruise mach.

    Also if the F-16XL cruises M1.1 at 20Kft then it must do close to M1.6 at 36Kft.

    None of the F-15s do Mach under 30Kft

    Many of the aircraft in the sixties could do this they just had **** poor SFC at mil and most had to be clean no missiles and used AB to get there, Lightning, F-104, Mirage III.

    http://www.f-16.net/forum/viewtopic.php?t=3491

    i cant find any solid information ( either flight manual graph or producer claim ) to show that they can supercruise with missiles , hence the reason i say they cant supercruise . And if we was to count relaxed supercruise then F-35 can do that as well ( 150 miles at mach 1.2 without afterburner )

    Your sentiment was which other 4th gen fighter can supercruise.
    Well there you are

    that wasn’t my sentiment either , you should read all the posts carefully to see who i was replying to , and what i meant
    Enzco posted this :

    F35 can not super cruise. What else do you need to prove this plane is not fast and will consume a lot of fuel ? I like the example of the neighbour wife. It is public that my neighbor wife can not go through my parking door. But then you Are telling us: that doesn’t prove the wife of my neighbor is fat. Ahahahaha

    then i replied with this :

    F-111 cannot supercruise, F-15 cannot supercruise, Su-27 cannot supercruise, mig-29 cannot supercruise, F-16 cannot supercruise, hell even Mig-31 cannot supercruise , are they all slow now?

    so it actually quite obvious that my post wasnt about ” no other 4 gen can supercruise ” but it is about ” just because an aircraft doesnt supercruise doesnt necessary mean it is slow “

    mig-31bm
    Participant

    So what if it “only” takes 20 years for radar technology to progress enough to be able to detect the F35 at useful range? (no right now it can’t, right?)

    Nic

    as radar improve, so is jammer, and a stealth aircraft will benefit significant more from jammer than a normal aircraft
    http://www.rfcafe.com/references/electrical/ew-radar-handbook/images/imgp88.gif
    http://forum.keypublishing.com/attachment.php?attachmentid=231760&d=1410975559

    in reply to: test pilot: "F-35 can't dogfight" #2157681
    mig-31bm
    Participant

    F-15E can supercruise, or an F-15 with the F229 engines.
    EF can supercruise with armament.
    Su-35S can supercruise with armament.

    And i mean supercruise without AB.

    And the Mig-31 can do a relaxed supercruise, it just get up the Mach numbers, throttle back to mil power, it will stay over Mach 1.0 for a loong time before it hit the transonic barrier and goes subsonic.

    I know the EF-2000 can do supercruise
    never heard of Su-35 or F-15E can do the same though ( of course iam open to the possibility that they can )
    about relaxed supercruise , we know F-35 can also do that , however EZo point is that any aircraft that cannot fly supersonic without afterburner is a fat , slow pig

    There is nothing unfair in that.. you always have the option to jettison the tank when the sh~t hits the fan..

    if you keep the fuel tank on , your RCS , agility ,acceleration , top speed , cruise speed decrease
    if you jestion it then your time in supersonic decrease , your combat radius decrease , there is no way around it

    In fact, it is unfair towards the F-35 that it always has to stay a fat slow pig at all times because it cannot jettison pretty much anything. Right, you have an EOTS aboard all the time, even if you don’t need one which renders it pretty much dead weight.. The bird is a conceptual disaster, nomatter how you look at it.

    I wonder why didn’t they simply make it smaller, lighter and mission reconfigurable. Put a cavity of standard dimensions into the airframe and develop modules – EOTS module, internal jammer module, additional fuel module, additional weapon bay module, whatever.. just like containers.. do you need to send six F-35s on a mission? right, two of them will take jammers, those two doing the actual attack will take EOTS and the escort aircraft take additional fuel, or additional pair of missiles.. You got everything you need, you retain full stealth and your aircraft are still light, nimble and agile.. a great concept would that be, IMHO..

    funny that you say that , because Rafale cannot jestion it’s IRST or internal jammer or pylon either
    and F-35 can dump fuel if needed

    mig-31bm
    Participant

    mig-31bm this is tiresome because you will selectively chose to answer only what suits you in a classic shill troll mode.

    I don’t usually bother because I know it will lead nowhere but what the hell….by the way it’s not you mig-31bm because I know someone else has written the recent answers for you ;D because you can’t or chose not to read what others have written because it doesn’t help your cause (you know whose!), have poor comprehension skills (to give you credit English is not your first language and you must be cheap to do rough and ready trolling (quantity and not quality in lots of “cut and paste” jobs that most people can’t usually be bothered to take to pieces!), and these recent answers are too fluent for you compared to your usual posts…..so my answer is to the remedial team that “helped with the “right” answers.

    Quick note to LM people helping mig-31bm with his answers…..why not let bring_it_on answer as he is infinitely more knowledgeable and Mr Brar is a true gentleman as well!

    Resort to name calling and insult when unable to win argument by logic or fact :rolleyes: but it ok , that what i would expected from a Rafale bot like you any way

    Where do I begin? I know: first stop lying and then repeating the same lie every few sentences….saying something over and over does not make it true!

    May be you should take your own advice and started posting fact instead of BS nonsense ? how about that ?

    In my earlier post I spelt out it was part development cost and part lifetime operating cost.
    Sorry, it’s you that doesn’t understand the numbers and haven’t (or can’t) answer questions posed after you cut and pasted a lot of complicated looking (but not complicated in reality) tables and graphs and had no reply to the fact the operating costs for the F-35 have been pulled out of the air t in three year’s time (mid-2018) because they aren’t real figures but just projections and guesstimates that aren’t worth the paper they’re written on…..on a small number of operational F-35s there is simply not enough data to give meaningful hourly cost rates….the data for the F-16C/D was culled over several years (2008-2010) and that won’t be possible for many years for the F-35.
    Secondly, the assumptions for some components of the hourly cost, such as maintenance may be understated by a wide margin….what if they are closer to $20,000 an hour instead of the $10,000 a hour figure? That will send the total program cost well north of $1.5 trillion won’t it!

    Perhaps Spudman can do the honours and do a costing where maintenance is $20,000 an hour and continued system improvement costs are many times (say $5000) the $1000 per hour used in the projection for mid 2018?

    Of course they are not real figure , they are estimated , how else would you get the cost of the whole F-35 fleet in 55 years ?
    you keep pulling the 1.5 trillions number and say it too massive and the development of counter measure would be cheaper , So stop dogging the question now let say you intended to counter the F-35 by using Rafale ,and it would take only 1 Rafale to counter 1 F-35 , how much would it take to develope , buy , operate ,and maintenance 2457 Rafale for 55 years ?
    you saying the maintenance cost of F-35 may be understated , how about others program ? how about Rafale ? how about Typhoon ? what make you think their cost isnt understated as well ?

    Just read the past few pages….the basic flaw is the constraint in using a single airframe to accommodate the Marines’ vertical take-off model F-35B, which is incompatible with Air Force and Navy requirements…..you get a short stubby fat pig that can fit on mini Marine carriers and this gives it the short legs that require massive tanker support to long range sustain operations….a senator might understand the analogy with Fatty Arbuckle or Oliver Hardy….both are surprisingly quick for fat men! ;D

    wow the Rafale bots are really all the same , F-35 have short range ? really
    You know what funny , your beloved Rafale would need massive external fuel tank to even match F-35 range , and while F-35 can peacefully doing strike or SEAD , your Rafale will have a hard time evade SAM and enemy’s fighters

    The point I was making was that countermeasures will be developed over time that will lessen any advantages due to LO,

    I have already explained it , weapon development will often benefit LO aircraft more than normal fighter
    better missiles ( more agile , more speed , multi mode seeker , smaller allow more missiles load ) ? => great for LO aircraft since they can shot first and can get closer for their shot
    better jammer ( more gain , more transmitting power ) ? => great for LO aircraft since burn-through range reduce significantly as RCS are reduced
    better radar ( more range , harder to jam ) ? => great since aircraft with bigger RCS will be detected from further , and stealth fighter can use the advantage in detection time to get into position for better missiles shot ( accelerate to fast speed or climb to high altitude )

    furthermore the developing of countermeasures will be relatively cheap compare to the total program cost of the F-35….that is why questioning the value for money….in plain English ‘is it worth it for what you’re getting?’, is a perfectly reasonable question.

    as i have repeated like a hundred times , 1.5 trillions dollars included development cost , the cost of whole fleet ( 2457 aircraft ) , the cost of operating and maintain that fleet for 55 years
    what would be the cost of your so called “counter measure” with same number , operating for exactly same amount of time ?
    say instead of buying F-35 , you bought Typhoon or PAK-FA or Rafale ..etc , how much do you think the fleet cost ( included everything )?

    Like the good little troll you are you just posted the KPP (chopping off the UK requirement at the end of the table!)

    feel free to post your ” un-chop” version then

    What is the point of posting this? We know what they are, but the point that you have avoided answering is that key performance parameters were relaxed so the F-35 could meet the required criteria! That was the whole point but a good troll just ignores it!
    !

    Firstly KPP is short for key performance parameters
    Secondly , If you talking about spec such as sustain G and acceleration time then go to this thread http://forum.keypublishing.com/showthread.php?135460-test-pilot-quot-F-35-can-t-dogfight-quot/page7 Andraxxus already made pretty reasonable and accurate explanation why F-35 isnt a pig as you troll like to call it

    in reply to: test pilot: "F-35 can't dogfight" #2157884
    mig-31bm
    Participant

    Why the hell do you want to remove the external fuel tank that is the standard configuration in supersonic? Is it because with the tank the F35 comparion is too embarrassing ?

    No, actually it opposite, if i including the fuel tank then i will have to hear MSphere moaning about how it is unfair for the legacy fighter since external fuel tank will increase RCS, reduce cruise speed , top speed, acceleration along with agility of Rafale, Typhoon .. etc and the like.

    mig-31bm
    Participant

    mig-31bm,

    First, you ignore the salient points that you can’t answer and then selectively bring in irrelevant points to cloud the issue.

    Your non-sequiturs and red herrings are designed to avoid answering the difficult questions and answering them removes the spotlight on the fundamental flaws.

    How big is the F-35 fleet, 130? It’s not big enough to get a handle on actual operational cost yet and when the fleet is big enough we can discuss this at the end of the current fiscal year.

    I’ll remind you of the main points that congress needs to know:

    No , you are the one who ignore the point and trying to cloudy the issue
    where do you think that 1.5 trillions USD number come from ? it not the cost of F-35 development , it is the price of the whole program and 55 years of service life for the whole F-35 fleet ( sustaining – maintaining ..etc )
    So you either measure the cost of the whole fleet around 2457 aircraft for 55 years or you measure the cost of 130 aircraft until now , if you want to talk about 130 aircraft then stop pulling that nonsense 1.5 trillions number

    ..

    The flaw in the F-35 is one air frame has to do different jobs for marines, navy and air force. The cost of $1.5 trillion isn’t worth it for what it does.

    And you know that how ? what is the evidence you provided to show that F-35 cant do the job ? or it not worth it ?

    If Lockheed Martin had to start again it would have a separate airframe for the vertical take-off version for the marines F-35B, and better performing versions for the Air Force and Navy.

    And that would make it more expensive , the whole point of the common airframe is to keep the cost down

    Forget trying to overcome S-400 and S-500 area denial missile systems, counter-measures to any new system as always will be adopted in iterative improvements to counter at a much lower cost…..the point being it won’t cost as much as $1.5 trillion to do that!

    you keep bring up that 1.5 trillions number without understand what it is :sleeping:
    it not the cost of the development state , it is the cost of the whole fleet , including operating sustaining , operating , maintaining over 55 years period ( inflation included )
    How much do you thing it will cost to develop , buy and operate a fleet of 2457 Rafale or Typhoon ( included things such as fuel tank and targeting pod as well )for the whole freaking 55 years ?
    And yes , better radar will be developed in future , better jammer will also be developed in future , better missiles will also be developed in the future
    however all of that affected all aircraft rather than just F-35
    better radar in future can see VLO from long distance will be able to see none stealth fighter from even further
    better jammer in future will help reduce radar tracking range will benefit stealth platform significantly more than a non stealthy platform ( reason have already been explained in previous pages )
    better missiles with longer range , better agility will benefit stealth fighter alot more since they can have first look , first shoot advantage

    Have I spelt out clear enough that it won’t cost $1.5 trillion to counter the F-35? (no degree needed to understand this fundamental flaw 😉

    you have make it clear that you dont actually understand the number.

    Because they cannot talk about its performance because key performance parameters were relaxed to make it meet the required criteria, they talk about the situational awareness, rubbish like it can see a rocket flare from 800 miles away, but so can mark 1 eyeballs!

    this is actual F-35 KPP
    http://1.bp.blogspot.com/-LQEZ-Yj5IOE/T1rOJND4KaI/AAAAAAAAB5M/M81SV0Lq8t0/s1600/2007KPPusedbyCRSin2012.png

    Its low visibility does not make it invisible to IRST and its huge F135 engine can be tracked….

    no aircraft is invisible to IRST , however IRST doesnt work well unless the weather condition is good or there is no cloud , for targeting IRST have to rely on LRF which have range of a little over 20-30 km
    To detect target at long range ,optical sensor like IRST have to focused ( reduce their FoV ) thus reduce SA significantly
    Last but not least, while F-135 is big , it have much higher bypass ratio than Snecma M88 , EJ200 ,or F119 , thus it will likely have lower exhaust temperature , leading to lower IR signature .

    All they can do to deflect criticism is to over-sell other aspects ,which in themselves are not directly linked to the actual aircraft, such as EODAS and situation awareness, which when it comes down to it is just the next iteration of sensors (EM, IR and optical and IR) which will also continue to improve over time to reduce any advantage at considerable less cost than the development of the F-35

    you have to consider the whole package rather than just the sensor alone by itself
    For example :
    if the 2 side use the exactly same radar , VLO aircraft will have significant advantage in detection range
    if 2 side use the same missiles , VLO will still enjoy higher PK shot since it can get much closer to target
    If 2 side use the exactly same jammer ,VLO platform can get much closer since reduce RCS also reduce burn through range
    ….etc

    in reply to: test pilot: "F-35 can't dogfight" #2157956
    mig-31bm
    Participant

    I am getting quite bored with this constant whining. Can you write something more usefui than the same tired crap with “show me the evidence”?

    Can you write something more useful than the same tired crap start with” f-35 is slow, not agile, useless… etc ” and actually write something based on logic or evidence?

    in reply to: test pilot: "F-35 can't dogfight" #2158126
    mig-31bm
    Participant

    Without taking drag and weight that is not in F 35 favor you are explaining that it is normal the F 35 do the same than 40 years old design that it supposed to replace ?

    and how long do you think Rafale, Typhoon , Gripen can stay at mach 1.6 without external fuel tank? ( since people always want to compare aircraft performance when clean)

    in reply to: test pilot: "F-35 can't dogfight" #2158129
    mig-31bm
    Participant

    Super cruise is not only about fuel consumption, it is about IR stealth. F35 doctrine is based on stealth. But it shine like a headlight as soon as it needs to go supersonic.

    every aircraft will shine when they go supersonic due to the sonic cone, F-35 is no exception, and F-135 have high bypass ratio which will give it lower exhast temperature
    http://www.f-16.net/forum/download/file.php?id=21202&t=1
    but problems of IRST is that for targeting they still have to rely on LRF which have range 20-30 km in good weather conditions

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