The weakest link of the B-1B design was its electronic suite, which made the swingwings look extremely inexpensive in comparison.
Back to my multiple booms. Anyone know why they stick to a single boom?
To be fair, the USAF does include space programs. Divide their budget in half and you get a fairly even set of programs compared to the army. The USN gets the lions share of funding, but they also have to account for 2/3’rd of the planet surface.
Bager1968-
Very reminiscent of the F3H Demon that came out of McDonnell. Almost looks like an F-4 lite. 🙂
Here’s my representation of F-18V, the stealth rhino…
The chinese killed by the strike were two specific journalists publishing less than glamorous stuff about NATO political leaders, not Tamara operators. I’m for certain the CIA knew what they were doing when they passed down these two positions, bypassing both the jfc and the informal jtcb at the time. Remember this is pre-jdtm we’re talking.
…And your sources for the Italian decision are?? Which Italian sources to you intend to quote?
My cousin Vinny said the 777 is luckier than all of the others combined. But looking at the big picture then one really ought to wonder why they are strapping themselves to a single boom. The requirement should contain an amendment concerning the need for multiple booms.
Considering air-intercept/air-to-air missiles are equivalent to drones then they already have motherships with 8-12 swarmers apiece available to them already. Otherwise it doesn’t make much sense to carry static aircraft like that. You are fighting gravity too much to justify the 99% of the time the planes are at peace-time status.
Surely someone has some more comparisons to make.
Who runs that MD-80 in the last frame as a tanker?
The F135 was designed for lower costs and fewer parts to maintain compared to the F119. You wouldn’t dare waste a well bred horse for plow work. You probably want the Lightning to be the plow puller and general work(-me-to-death-)horse while the Raptor is good for running to town on Sundays.
The low chord wing offers all around performance during peace-time conditions superior to the cranked wing of the F-16XL. So for 99% of every F-16’s life-time the low chord wing is the better choice. If they had to lug around so much more drag in their wayform then imagine the fuel costs over twenty years.
Why would they waste time trying to add low observability to a flying reflector the size of a barn? If they were going to reduce its rcs then they’d need a much more drastic redesign then simply changing a few shapes on it. The materials alone used in its construction would need to be largely rethunk.
I’d certainly hope they were running non-a-b at 60,000 feet. The U-2 never needed a-b for a reason. Think lean.
A straight shooting 30mm built into a helicopter makes no sense when they have gunpods that already do it.