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MadRat

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  • in reply to: Embraer KC-390 rolled out #2215077
    MadRat
    Participant

    When I saw the probe it made me think…

    http://cdn-www.airliners.net/aviation-photos/photos/9/3/6/1332639.jpg

    in reply to: High bypass drop tank-integrated turbofan #2215079
    MadRat
    Participant

    Hound dog was interesting
    http://www.strategic-air-command.com/missiles/Aircraft-Launched_Missiles/images/agm-28b.jpg

    in reply to: High bypass drop tank-integrated turbofan #2215225
    MadRat
    Participant

    No, not switch off any motors. Instead using a lower cost turbofan to extend the range and endurance of these fighters.

    The B-52 throttles down to about 4000 pounds of thrust on cruise on an engine that maxes out at 17k pounds.

    Centerline is a no go on the F-16CJ. It’s only a 300-gallon fixed tank that is too short for the FJ-44. The numbers are relatively thin on the 370-gallon sized tanks. It pretty much requires the 600-gallon sized tanks.

    It might not work out with FJ-44, it’s just an example which had an easy to find sfc. It’s a common engine. And it’s relatively low cost. There is always the stealthinized Williams F112 used in cruise missiles with a maximum thrust at 1k pounds at an sfc range between .2 and .25 depending on the settings.

    in reply to: High bypass drop tank-integrated turbofan #2215295
    MadRat
    Participant

    It’s difficult finding specifics on the F-16CJ. Internal fuel is 6970 pounds. External fuel can be accomplished many ways.

    Centerline can be a 300-gallon fixed tank with optional wing tanks of 370-gallon capacity.
    Or option for two 600-gallon drop tanks for ferry flights. Optional 300-gallon centerline tank in this configuration.
    The CJ does not support the removable conformal fuel tanks.

    Fuel consumption numbers on the web are all over the place with the crazy notion peak endurance for an F-16CJ is attained at Mach 1.4 at flight level 360. That sounds crazy. The manual cites Mach .87 optimally for 5000 pounds or more fuel above FL 400. It drops to Mach .45 at sea level and under 2000 pounds remaining.

    in reply to: RuAF News and Development Thread part 13 #2215297
    MadRat
    Participant

    What would they do, convert to an X2 setup with counter rotating blades and a pusher prop? IDK. Would impede ramp operations.

    in reply to: RuAF News and Development Thread part 13 #2215303
    MadRat
    Participant

    K’s seem like full versions accepted for export.

    E’s seem to imply neutered.

    in reply to: Military Aviation News-2014 #2215363
    MadRat
    Participant

    Air Force strike chief urges B-52 engine replacement

    Sharing engines with C-17A can only help.

    in reply to: High bypass drop tank-integrated turbofan #2215420
    MadRat
    Participant

    Fuel is under eight pounds per gallon. The FJ-44-4 would need a weight offset of 90 gallons, not 148 gallons per engine. And it puts out an advertised thrust of 3500 pounds st. The engine can get you up to Mach .85, whereas you said Mach .77 was the limit. That’s perhaps the design speed of the Citation, but that isn’t necessarily the limit of the engine.

    in reply to: High bypass drop tank-integrated turbofan #2215675
    MadRat
    Participant

    I’m looking for net gain per drop tank, so for an F-16 it wouldn’t really be feasible except on the F-2A which has the bigger wing and supports bigger under wing stores. It would make much more sense on the F-15E, but at still a modest gain. The F-16CJ at most would be around 8% gain on a centerline 370-gallon tank. It would exceed double digits on the F-15E.

    The real difference is it offsets any drag induced by carrying the drop tanks.

    in reply to: High bypass drop tank-integrated turbofan #2215728
    MadRat
    Participant

    If you have an F-16CJ with a 370-gallon equivalent powered drop tank you could conceivably get away with a 2500-pound static thrust FJ-44 at 500 pounds dry weight. That would offset around 70-80 gallons of fuel. That 2500-pounds of dry thrust is at .45 SFC as opposed to the F100’s .90-ish SFC. That’s approximately a X% boost in cruise efficiency at worst. It may be up to Y% but I’m only guessing at F100’s best cruise setting. And. the boost comes at the mere cost of 20% of the fuel in the external tank, which the FJ-44 can still cut further into the efficiency curve by continuing to burn internal fuel.

    That’s a substantial boost that only grows with a larger FJ-44. The offset of fuel is more than made up for in the efficiency boost.

    edit: My X% and Y% off by quite a bit after review. At best it might gain single digit boost over the fuel offset in the drop tank. Well, after further review it doesn’t work out so well on the 370-gallon tank. The SFC of F100-pw-100 is .76 and the newer versions go up to .745 sfc. That puts a big hole in the plan for a smaller tank. You need the 600-gallon tank to approach much gain for a large investment in time and energy.

    in reply to: A Tiger with powerful claws #2215823
    MadRat
    Participant

    With all the micro-turbofans in the J85 size I am surprised there has been no second wind program to squeeze another life out of them. The F-5 has been super adaptable as the design has been customized by about every user out there. The EM is yet more proof of that.

    in reply to: Saab Gripen & Gripen NG thread #3 #2216094
    MadRat
    Participant

    Gripen with Typhoon pictures are common. Gripen shows up with Hornet and Superhornet a lot, too. Gripen gets around quite often. Just not with Rafale. I think Rii is on to the game.

    in reply to: Saab Gripen & Gripen NG thread #3 #2216172
    MadRat
    Participant

    oh and i’ve got a number of Rafale and Gripen photos shot at various airbases over the years.

    So instead of producing evidence you’re getting confrontational. I get it.

    in reply to: Saab Gripen & Gripen NG thread #3 #2216305
    MadRat
    Participant

    Because it certainly is a rare event for the two of them to be in pictures together.

    in reply to: F-35 News, Multimedia & Discussion thread (3) #2216465
    MadRat
    Participant

    The S-3 Viking used a maritime version of the same turbofan, so it’s not exactly impossible for a Marine A-10. Just unnecessary when F-35B is so close to IOC.

Viewing 15 posts - 1,066 through 1,080 (of 4,651 total)