That I was expecting.Tilt nacelles are significantly shorter too. Guess it eases storage and airlift.
Not a clue. I would have thought that the Blackhawk like fuselage was pretty tough, though.The boxier fuselage is a surprise Scott Kenny, I did not expect that with the Valor. Is the redesign to do with surviving hard landings?
Gonna be hard to armor that, barring maybe a big plate to the front to cover the exposed area.I'm excited to see what solution they come up with to protect the guts of the nacelles from small arms fire.
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Maybe to provide a bit more internal space?The boxier fuselage is a surprise Scott Kenny, I did not expect that with the Valor. Is the redesign to do with surviving hard landings?
An armor plate attached to the moving part would work better and be more aerodynamic when in flight mode.Probably just blankets for small arms.
Still seems weird that the fuselage is now boxier than before, and not with a midlevel chine for RCS or anything.Recall that the V-280 was design to course basic parameters, where as this aircraft is being designed to specific requirements.
I would assume that after they won the contract, Army approached them and asked if they could fit some specific piece of equipment into the cargo space, Bell responded they can do it if they reshape the fuselage, and Army went: "Great, do that then."Still seems weird that the fuselage is now boxier than before
Oh, agreed, it's just odd that this requirement wasn't mentioned during Prototype.I would assume that after they won the contract, Army approached them and asked if they could fit some specific piece of equipment into the cargo space, Bell responded they can do it if they reshape the fuselage, and Army went: "Great, do that then."
I don't know what it would be, but the Valor has significant load carrying capacity, the ability to carry a lot of things is definitely limited by internal volume/shape.
Ah, makes a bit more sense now.For the record the prototype is what is being deigned now. V-280 was a technology demonstrator.
Again still early stages. Look at the pre production models and prototypes for nearly every plane.Ah, makes a bit more sense now.
Still seems weird that the outer fuselage mold line is an Amazon Box with wings. I would have expected at least some level of radar chines.
It's certainly going to redefine planning for our opponents... Going from "The US has helicopters that can do 100 knots loaded over a ~50 mile radius" to "The US has tiltrotors that do 300 knots loaded over a ~150 mile radius" is going to complicate their defensive schemes for a long time.AW&ST (Tony Osborne) has an interesting article up (link below). While it is much more than a V-280 article I thought I would post the salient points about the FLRAA program here for discussion.
"The reverberations from the U.S. Army’s decision to select Bell’s V-280 Valor for its Future Long-Range Assault Aircraft program are likely to be felt by the global rotorcraft industry in the coming years.
While the decision will change the shape of the helicopter industry in the U.S., the Army’s push toward a higher-speed rotorcraft now looks set to drive a recalculation in the planning, doctrines and requirements for helicopters among U.S. allies.
...The U.S. Army’s choice is arguably an epoch-defining moment for military rotorcraft. It may prove even more significant than the introduction of the turboshaft engine onto helicopters in the 1960s, which transformed their performance. Indeed, the selection of the Future Long-Range Assault Aircraft was probably the highlight of what would have been yet another quiet year for the helicopter industry."
https://aviationweek.com/defense-space/aircraft-propulsion/growing-rotorcraft-industry-faces-regulatory-supply-chain-issues
It's certainly going to redefine planning for our opponents... Going from "The US has helicopters that can do 100 knots loaded over a ~50 mile radius" to "The US has tiltrotors that do 300 knots loaded over a ~150 mile radius" is going to complicate their defensive schemes for a long time.
That's how it always goes. Removing the swoopies is how you make it cheaper.Found on X. Model shows the revisions to the design. As expected; less swoopy.
GBAD is easier, but ground army planning just got a lot uglier, since the US can now move a battalion 150 miles or more in half an hour.In terms of GBAD that's barely a noticeable change. In fact it could make their life easier without the Doppler confusion that helicopters can cause. And the RCS of those massive props...
All that orange wiring is test instrumentation. Once they confirm that engines are performing smoothly, that orange wiring will be deleted from production examples.I'm excited to see what solution they come up with to protect the guts of the nacelles from small arms fire.
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Also, I would imagine that the Army has pointed out to Bell that the open nacelle might be worthy of further consideration.All that orange wiring is test instrumentation. Once they confirm that engines are performing smoothly, that orange wiring will be deleted from production examples.
Sure, test instrumentation is always orange. However, V-280 is a technology demonstrator. The prototype aircraft that will later become the production version will be completely different, including different engines!All that orange wiring is test instrumentation. Once they confirm that engines are performing smoothly, that orange wiring will be deleted from production examples.
I'm still expecting a bulletproof panel covering the hinge so that only shots from directly below can get in.Also, I would imagine that the Army has pointed out to Bell that the open nacelle might be worthy of further consideration.
Bluntly, if you aren't having your end users doing their usual things with your prototypes, you're screwing up.First FLRAA Soldier Touch Point Successful
Program Executive Office, Aviation conducted a Future Long Range Assault Aircraft Soldier Touch Point the last week of November at the Bell Flight Research Center in Arlington, Texas.www.dvidshub.net
Bell requested soldier-touch-points before the program award. I believe they had three. These really assisted, especially with the maintainability of the platform.
Issue was never with forward ejection, issue was gas port sizes. Took some work on the engineers side, but the retests on InRangeTV showed 100% reliability with only 3x settings: Normal, Adverse, and Suppressed.Did they genuinely fix the issue with the forward ejection on that mdr?
That's nonsense. The CV-22 is over 18 feet high when folded. The maximum a C-5 will take is 13'6".Just one of those guys that looked at the accident record of the MV-22 during development and early operational introduction and utterly refuses to accept the reality that those accident rates (which were already lower than what the CH-46 had experienced) have been significantly reduced in the 15 years it has been in operational service.
But he does have a point that you were trying to present the V-280's unfolded height & footprint as the representing the final production product... when ALL of the information released shows that production V-280s will have folding capability for at a minimum air-transport, and most-likely normal operational use (just like the USAF's CV-22As all have folding capability despite not seeing the deck of an LHA/LHD except during very specific training scenarios).
The USAF specified folding capability just for air-transport of their CV-22As - just as the US Army will for its V-280-derived combat aircraft.
My understanding is that one of the critiques of this program is that because the aircraft can't fit in a C-17, like the V-22 it has an self deploy requirement which is loosely California -> Hawaii without refueling.
While no doubt doable, my best wishes (and condolences) to to the crew
I would not call that a critique so much as an asset. The Army specifically wanted an aircraft that can self-deploy in the Pacific without relying on airlift, which is slow and will be in high demand for other cargoes.
Strategy should inform capabilities, and capabilities drive requirements.Current Army aircraft have a radius of action of 90-100NM. This is completely inadequate for the Pacific, not even discussing the self-deployment requirement.
Not island hoping? I don't think one gets to decide that.