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LowObservable

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  • in reply to: Saab Gripen & Gripen NG thread #3 #2302870
    LowObservable
    Participant

    A Turkish-Korean-Swedish fighter?

    Will it be delivered in a flat-pack with a wordless instruction sheet and an Allen key?

    in reply to: F-35 debate thread. #2303796
    LowObservable
    Participant

    “Combat range”, as defined in Spud’s Lexicon: “Range achieved in any configuration where the F-35A has an advantage.”

    On the other hand, if I compare F-35A and F-16 combat radius with the same weapon load and mission profile, and with cleared take-off weights, the F-16 is comparable or superior despite being much smaller.

    in reply to: F-35 debate thread. #2310914
    LowObservable
    Participant

    Spud – Would you care to review your many posts and comments over the years, and figure out how many times you have said “this and that will happen in 20xx” and how many of those predictions have been accurate?

    The risk mechanism in excessive concurrency (and the entire Pentagon leadership now accepts it was excessive) is that the goal in the process of transitioning from DT through OT to operations is to get fully operational jets to the squadrons.

    So when it comes to modernizing pre-IOC-standard jets, the lowest cost and fastest payoff is to start with the newest aircraft, which need least work and have most lifetime left, and then work backwards through the production numbers. The result is that you end up with a rump of old airplanes that need a lot of work – which is where 40+ F-22s are stuck today.

    Bogdan made it clear the other day that they are trying to get the concurrency problem tamed, but I would not bet any money on when jets before Lot 3/4 get upgraded to full combat capability.

    in reply to: F-35 debate thread. #2318900
    LowObservable
    Participant

    Rii – 😀

    As for modern fighters:

    T-50 is classic-Ferrari great-looking.
    The Su-27 to -35 family is not exactly beautiful, but totally badass.
    The Typhoon is muscular, like an Aston, and the Rafale is one of Citroen’s better efforts. More Moreau than Bardot, to go in a different direction.

    The F-22 and J-20 are OK in proportion, although the vertical stabs do nothing for the Raptor’s looks.

    The F-35 from most angles looks like Rosie O’Donnell in yoga pants. You may disagree if you wish, but you will still be wrong.

    LowObservable
    Participant

    Is there any evidence that CUDA exists beyond resin models and briefing cards? Where is the tech demo plan for a compact HTK seeker and a flight control system never used before on an AAM or a missile this size? How long will that take and how much will it cost? What’s the real projected performance?

    And when did anyone at LockMart last design an AAM? Neither LM nor its legacy companies were involved in the last two US competitions for an all-new AAM (AIM-9X and AAAM).

    On the other hand, it’s interesting that a jet that is 600 per cent better than all others (except F-22) in air-to-air suddenly needs to carry twice as many AAMs as we previously thought that it did.

    LowObservable
    Participant

    Spud – It’s a bit more than that.

    In operational use, the engine would be expected to hang together given regular inspections by line maintainers, and it would be a BFD if a critical component was found to be AOG-damaged ahead of prediction. That’s why they do testing.

    Well, maybe this is a manufacturing anomaly, but if so, it’s the second such in the F135 since the NYE corks popped, so the root cause analysis should be entertaining.

    Note also that there have been headaches and redesigns with this turbine stage before, and that it is designed to unique requirements because most of the STOVL-mode thrust comes off the LPT.

    And I bet that the program leaders and flacks SO wish that right now they could be saying: “However, flight sciences, mission systems and training of the F136-powered aircraft continue normally.”

    LowObservable
    Participant

    Diagnosing anti-Americanism as “racism” is a bit of a stretch given the number of ethnicities resident in the US population. But that’s why people are on my Ignore list…

    LowObservable
    Participant

    There is AFAIK no definition of LO/VLO/ELO that has any agreed, universal or official acceptance.

    This is not surprising.

    The RCS characteristics of every platform are different in degree, bandwidth and aspect-dependence, so summing them up into a single LO score would be (a) difficult, (b) pointless and (c) require whoever is doing the scoring to have an altogether dangerous degree of access to sensitive data for multiple platforms.

    Also, the term “LO” is properly applied to the technology (eg in terms like CLOVerS and LO-EXCOM) and would be confusing as a platform description.

    LowObservable
    Participant

    Hardeharhar.

    Obviously impossible to estimate RCS from 3D models based on photos. That’s why F-117 and B-2 shapes were revealed so early.

    Funny how some people are technically skilled programmers one minute, and can’t be expected to explain the most basic concepts the next.

    LowObservable
    Participant

    Well, Spud, you have me stumped on that one, because I have no idea how something like EO-DAS can do passive ranging to a moving target on its own, because there ain’t no range data in a receive-only signal, and that’s not just a good idea, it’s the law. All I have is Az-El and magnitude.

    A fixed off-boresight target, maybe – calculate the rate of angular change. IRST can use dynamic ranging against a head-on target (lock-on, make the airplane weave, triangulate) but not something you’d take to the bank.

    Multiple platforms – well, everything’s possible provided you’re willing to accept that you just squared all your ambiguities.

    So since you brought it up, why don’t you explain how it works?

    LowObservable
    Participant

    Picard/MC – IIRC the issue is that the wavelength of the RF radiation is changed in the RAM. So yes, you may need wavelength-related depth, but the wavelength is not the same as that in space or free air.

    Spud – Can you explain how the supposed “internal CPU” in EO-DAS “geolocates” anything on its own, based only on relative Az-El data?

    Geolocating a terrestrial target would require at very least a digital terrain model and platform position and attitude (it actually requires more than that because tiny errors in sensing are big errors on the ground). Determining a position for an airborne target would require two platforms triangulating one another or the use of radar.

    LowObservable
    Participant

    That book is dated 2006 and the information about the dual-band DAS, I believe, is much older than that. It’s been a 1 MP FPA for donkey’s years.

    And of course there are processors in the units and DAS SW that does the tracking. Does not mean that they are in the same place.

    LowObservable
    Participant

    Northrop Grumman describes DAS as the only 360-degree, spherical situational awareness system in existence today. Comprised of [sic] six mid-wave infrared cameras located on the forward and center fuselage of the F-35, DAS can warn JSF pilots of incoming aircraft and missile threats, provide 360-degree day and night vision, fire control capability, and precision tracking of wingmen/friendly aircraft for tactical maneuvering.

    When the system detects a missile or aircraft, DAS provides the detection information to the F-35’s sophisticated suite of mission systems, known collectively as its integrated core processor (ICP). As Dave Bouchard explains, the ICP or what he refers to as the F-35’s “fusion engine,” then fuses the information.

    “All mission systems sensors in the F-35 input to Lockheed Martin’s fusion engine. Ultimately, the fusion engine determines the outcome. It’s not that the radar will do this or DAS will do that. The radar and DAS input information into Lockheed’s fusion engine and then that system provides the answer or output. DAS is a key player in the entire kill-chain with the system being on the front end.”

    http://www.defensemedianetwork.com/stories/front-end-of-the-kill-chain/

    Spud, can you point to where IIR FPA pixel pitch can be reduced? You’d have to do that in order to provide higher resolution in the same size unit, This paper…

    http://client.blueskybroadcast.com/spie/dss08/6940-95-a7c_maillart/manuscript.pdf

    .. suggests that there’s a diffraction limit that starts to cut in at 15μm because you’re basically bumping into a pixel size that is close to the wavelength of IR radiation.

    Actually, there’s probably more mileage to be gained with dual-band technology.

    LowObservable
    Participant

    19 MP per camera would be nice for video to show later, but could start to cause you a little difficulty latency-wise. 114 MP is kind of a lot to process in real time. 1 MP it is.

    Bluewings – I’m sure the system has its uses, but the idea of using EODAS tracks only (that is, any tracks outside the field of regard of the radar, EOTS or meat-servo helmet) to go shoot things is a bit scary.

    LowObservable
    Participant

    Do I work for NG?

    Really, Aurcov.

    Hot things in the sky? Well, there are a lot of white things that reflect solar IR quite efficiently.

    EOTS can give you some idea of ID as long as the target cooperates by staying below or just above your waterline.

Viewing 15 posts - 616 through 630 (of 954 total)