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stealthflanker

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Viewing 15 posts - 766 through 780 (of 781 total)
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  • in reply to: RuAF News and development Thread part 14 #2183887
    stealthflanker
    Participant

    b.t.w., is the AL-31FM1 on Rusoboro export list?

    As far as i remember no. Only the F, FP and FN that being offered.

    in reply to: RuAF News and development Thread part 14 #2183911
    stealthflanker
    Participant

    hmm what engine did Su-30SM used ? Similar type as the export (AL-31FP) or newer AL-31FM ?

    in reply to: Su-35 versus F-35 in command sim #2183921
    stealthflanker
    Participant

    if rad base didnt factor in surface wave diffraction then RCS at 1 Ghz would be lower than 10 Ghz , which is clearly not what they showed in their simlation

    It is lower and the “beamwidth” become broader. Don’t you noticed it ? Please look again at your Graph. Look at the “Blue” Line (1 Ghz) Thus why when the first time i saw that graph i concluded that the software only calculate specular RCS but later from the technical brochure i found it’s also do Multiple edge scattering and Edge diffraction.

    The edge diffraction one however is the one i doubt that it will include surface wave and creeping wave.

    in reply to: Su-35 versus F-35 in command sim #2184310
    stealthflanker
    Participant

    For the Su-35S – the problem of polarisation caused by the rotating swashplate (the IFF is an AESA not a PESA).

    Where i can read more about this ?

    For the PAK-FA it works independently of the main AESA interrogating passive ESM tracks and which (imho) assists in designating the targets’ spatial location – hence giving the pilot a relatively accurate real-time picture of the battlespace without going ‘active’ in X-band.

    This is the point which does not make sense to me. Are you saying that when the ESM detects something… the Interrogator array will then point its beam there.. Emit and then wait for reply ?

    Thats quite obvious. They need the volume of X-band radar array for.. here it comes; T/R nodes.

    Those L-band slats array are quite large(relative), how on Earth can you fit them on the IRBIS-E array..?

    For the record, i think this is an clever solution indeed. So why do you think otherwise?

    Well the IFF array doesn’t have to be that big for the starters. Thus i think there won’t be any problem embedding them into the main array as the earlier Russian ESA’s.

    So i think the L-band array is able to do something more.

    in reply to: Su-35 versus F-35 in command sim #2184424
    stealthflanker
    Participant

    Well, you should ignore those people:

    http://kret.com/en/news/3527/

    I don’t mean to be rude, but it’s very difficult to *debate* with someone when the very foundations of their argument are often proved factually incorrect and are sometimes nonsensical.

    still wondering though.. why they can’t just install it in the main array.

    (Already browsed the older thread but some points doesn’t make sense to me, especially the whole “IFF tracking” stuff)

    in reply to: Indian Air Force Thread 20 #2184614
    stealthflanker
    Participant

    Greetings 😀

    got a question.. Given that Indian airforce operate very diverse inventory of aircrafts, i wonder how Indian airforce integrate all those aircrafts so they can share situational awareness or even directing fire? Like say datalink, can Indian Mirage-2000 share data with Su-30MKI ? Or can the A-50EI AEW/C share its radar picture to Mir-2000 ?

    thanks for any response given.

    in reply to: Russian Navy Thread 2. #2020408
    stealthflanker
    Participant

    Hello all :3 quick question.

    Why S-300F..or early variant of it use 3R41 Volna ?

    http://farm5.static.flickr.com/4096/4934505320_b235e3aeb8.jpg

    Unlike its land S-300P sisters. Volna is a reflective type ESA where the feed horn is placed at the front of the antenna. Im also see similar trend at Klinok and Orekh. Why those systems don’t use (except at Peter the Great where it has a 30N6 replacing one of 3R41) Backplane feed as its land based system ?

    in reply to: Su-35 versus F-35 in command sim #2184728
    stealthflanker
    Participant

    edge diffraction is used to talk about reflection due to surface wave, when you you illuminating something directly and get reflection, then they would simply call it spectacular return

    Specular return does not have spherical pattern.

    http://oi62.tinypic.com/11rq1eb.jpg

    early 1980’s Fuhs lecture do separate edge diffraction with those originated from surface travelling wave.

    in reply to: PLA video shows China defeating the US #2184737
    stealthflanker
    Participant

    More like another Chinese animation studio showcasing their 3D skills. Which is awesome.

    No need to take it seriously.

    in reply to: Su-35 versus F-35 in command sim #2184789
    stealthflanker
    Participant

    edge diffraction is the result from surface wave

    It can also be caused by direct illumination of the tips/edges by EM wave.

    in reply to: Su-35 versus F-35 in command sim #2184819
    stealthflanker
    Participant

    that probably due to the fact that reflection from surface wave is much lower than from spectacular return, thus they beng overlapped in the graph

    Or it’s not considered. Found the rad base brochure here :

    It’s simulation includes

    · Blocking
    · Multiple Bounce Interaction
    · Edge Diffraction
    · Polarization
    · Dielectric Materials
    · Bistatic Computations

    https://www.scribd.com/doc/278284451/RadBase2-Tech-Paper

    in reply to: RuAF News and development Thread part 14 #2184829
    stealthflanker
    Participant

    http://www.armstrade.org/includes/periodics/news/2015/0903/124030946/detail.shtml

    So, Indonesia has decided to buy the Su-35, though in batches as the budget allows.

    Don’t hope too high for this.

    Our Govt has quite a record of boasting stuff without realization.

    in reply to: Su-35 versus F-35 in command sim #2184863
    stealthflanker
    Participant

    They also use Chu Stratton integral method which can be used to measure diffraction from surface wave

    Then i wonder why their polar plot somewhat only depicts Specular RCS result.

    Let’s try computational electromagnetic simulation of an F-22, shall we?……….’oh oh spaghettios’!!:

    https://www.google.co.jp/url?sa=t&source=web&rct=j&url=http://www.ijrame.com/vol2issue1/V2i105.pdf&ved=0CB8QFjAAahUKEwjfnubq59vHAhVEPhQKHTTlDeU&usg=AFQjCNGlPzhSPjv-SAVP3qsUUTChB4OvGg&sig2=3ptES2xxLChWF76-OhN5vQ

    The most interesting aspect in that paper, for me at least is NOT their RCS measurement but their derivation of radar range equation. One can actually find out its detection range in various band if having a “reference range” It’s basically 4th root law but using frequency.

    It basically state that VHF Band radar will have 7-8 times detection range of X-band (assuming same gain etc..Only frequency change) L-band will have 2 times detection range compared to X-band.

    How to use calculate that ? The paper doesn’t mentioned it but i figured out myself.

    Reference band : 10 GHz =10000000000 Hz
    Reference range :30 Km

    We want to calculate range at VHF Band (175 GHz). We need to find the detection range “factor” of the reference band first

    range factor for 10GHz : SQRT(1/10000000000)

    Range factor would be : 0,00001

    Then we find range factor for the VHF band

    0.175 GHz = 175000000 Hz

    range factor for VHF : SQRT(1/175000000)

    Range factor would be : 0,0000756

    Then divide the range factor of the band we intend to calculate with reference range factor :

    0,0000756/0,00001 = 7.6

    Thus the 175 MHz radar will have 7.6 times range of the X-band radar or 7.6 * 30 = 226.8 Km.

    in reply to: Su-35 versus F-35 in command sim #2185202
    stealthflanker
    Participant

    Here it is

    http://aerosim.calpoly.edu/media/cms_page_media/14/Vendetta%20-%20Final%20SAWE%20Paper_1.pdf

    Thanks.

    and yes, it’s modeled using Physical Optics method. Thus it does not model RCS increase from Surface Travelling Wave and creeping wave.

    ————–
    Anyway regarding to RCS dependency on wavelength squared though.. I remember page 59 from Knott and Schaeffer (RCS 2nd Edition) That a vehicle designed for low RCS at 10GHz will have additional 18Db RCS at 1.25 GHz. Nonetheless it mention no mathematical equations.

    in reply to: Su-35 versus F-35 in command sim #2185521
    stealthflanker
    Participant

    I’ll have to find the original source, but here is a graphic from a university study. Keep in mind that no RAM was used and only shape was considered. It’s also a generic airframe that conforms to normal VLO design precepts (no right angles, continuous curves, etc).

    Note that the differences between 1Ghz (UHF/L Band) and 12Ghz Ku Band) are not that great.

    http://i.imgur.com/B1ESHa0.png

    Would love to see the paper.

    From what i see however.. That RCS polar plot only consider specular RCS spikes. While low band radar’s “counter stealth” mechanism relies more on resonance and creeping wave. Those two mechanism that will add RCS.

    Specular RCS from what i know kinda behave like “antenna beamwidth”. Having similar “wavelength/antenna dimension” relation. The larger the wavelength the weaker the lobe BUT it’s getting broader. While smaller wavelength will produce a very sharp and strong but narrow lobe accompanied by weaker “sidelobes”

Viewing 15 posts - 766 through 780 (of 781 total)