![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]()
Scott Ferrin wrote:
On Wed, 03 Mar 2004 03:19:41 GMT, "Thomas Schoene" wrote: Scott Ferrin wrote: Nope. The X-32 would have but not the 35. My guess is they could have but maybe Lockhhed didn't want it competing with the F-22. Or they didn't want to pay the weight penalty in an aircraft designed for strike over air-to-air. I recently suggested that if the F/A-22 were canceled, the Air Force might look at an air-to-air version of JSF. An axi-symetrical thrust vectoring nozzle would be high on the list of desirable modifications for such an aircraft, I suspect. I'd think they'd have to make quite a few changes to make it good enough to be the primary air to air fighter. Internal weapon load is tiny (2 -120s) But the bays also have space for a pair of 2,000-lb bombs. If you can't find a way to get another AMRAAM in each bay, you're not trying. Two more in each bay would be harder, but seems doable. A total load of four AMRAAM woudl be small, but acceptable. A toal of six would match the F/A-22. , the thrust to weight leaves a lot to be desired, The F135 is officially a "40,000-pound class" engine, against a max-fuel weight of just under 50,000 pounds. Depending on how much rnage that thrust actually covers, the plane has a max-fuel thrust:weight of around 0.8:1 to 0.9:1. With less fuel (say partway through a flight) it might approach 1:1. (And as Kevin says, taking out the bomb rakcs would help a lot) As a real widlcard, Rolls Royce says the F136 can put out 56,000 pounds of thrust. If that number is even remotely close to right, there's a lot of surplus power potential there. Might have to rethink the inlet design, but that's not impossble for a dedicated air-to-air variant (certainly cheaper than a new plane). http://www.paksearch.com/br2002/Jul/...%20have%20huge %20thrust.htm and how does it fair in the manueverability dept.? (Fare) The Air Force says its instantaneous and sustained g capacities are already comparable to an F-16. They don't say which version of the F-16 or under what loads, but it's a hint that maneuveravility are not too bad. Sure you can add external weapons but then there goes your stealth. Well, there are degrees of stealth here. Wingtip AIM-9Xs might not impose horrible RCS penalties. -- Tom Schoene Replace "invalid" with "net" to e-mail "If brave men and women never died, there would be nothing special about bravery." -- Andy Rooney (attributed) |
#2
|
|||
|
|||
![]() But the bays also have space for a pair of 2,000-lb bombs. If you can't find a way to get another AMRAAM in each bay, you're not trying. Two more in each bay would be harder, but seems doable. A total load of four AMRAAM woudl be small, but acceptable. A toal of six would match the F/A-22. I was thinking more about the cost to make the changes. I suppose it would matter WHEN the F-22 got cancelled so they could make the changes upfront. , the thrust to weight leaves a lot to be desired, The F135 is officially a "40,000-pound class" engine, against a max-fuel weight of just under 50,000 pounds. Is that with no external stores? Depending on how much rnage that thrust actually covers, the plane has a max-fuel thrust:weight of around 0.8:1 to 0.9:1. With less fuel (say partway through a flight) it might approach 1:1. (And as Kevin says, taking out the bomb rakcs would help a lot) As a real widlcard, Rolls Royce says the F136 can put out 56,000 pounds of thrust. If that number is even remotely close to right, there's a lot of surplus power potential there. Might have to rethink the inlet design, but that's not impossble for a dedicated air-to-air variant (certainly cheaper than a new plane). Yeah I've been hoping that's more than a pipedream on RR's part. Apparently they say they're real numbers though. I know the X-32's engine hit 52k in max AB. and how does it fair in the manueverability dept.? (Fare) The Air Force says its instantaneous and sustained g capacities are already comparable to an F-16. They don't say which version of the F-16 or under what loads, but it's a hint that maneuveravility are not too bad. I wouldn't be surprised if they were downplaying it either. Back in the early days of the F-16 they didn't exaclty encourage comparisions to the F-15 for fear of not being able to buy all the F-15s they wanted. Sure you can add external weapons but then there goes your stealth. Well, there are degrees of stealth here. Wingtip AIM-9Xs might not impose horrible RCS penalties. Hard to say. In Ben Rich's Skunk Works he related an incident where one screw not completely tightened down made the difference between not being detected and EASILY being detected on Have Blue. ISTR the screw protruded 1/8". And that's with late 70's radar. Then again there were some pretty glaring goofs in the book so who knows? |
Thread Tools | |
Display Modes | |
|
|