MasterBates
Well-Known Member
It will take a hi viz fatal mishap to get a COD replacement, or the NP2K properly fixed.
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I have heard the the V-22 can't fit a hornet engine inside. That was one of the big show stoppers for the "Clopter" (Carrier Plopter)
What's the weight of a hornet engine? If anything I would think that could be a limiting factor.
Navy or Air Force?Actually, it's the airspeed velocity of the unladen Osprey.
What's the weight of a hornet engine? If anything I would think that could be a limiting factor.
What's the weight of a hornet engine? If anything I would think that could be a limiting factor.
I'm sure the Marines have this figured out already for the Osprey. The C-2 NATOPS has a large list of engines and under what conditions we can transport it (in the can, on a cart, sections, etc). When a new engine hits the fleet, they bring one to the hangar and load it into the COD to prove if its possible or not. I was there when the Pax folks did that with the Super Hornet engine and I've heard it was done with the F-35 engine mockup.
It will take a hi viz fatal mishap to get a COD replacement, or the NP2K properly fixed.
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Couple buddies of mine almost witnessed that. Someone (like presumably the air boss) was apparently yelling at them to "eject" as they settled heavily off the cat (like kicking up a rooster tail of saltwater low). After they were climbing away and everyone got their seat cushions out of their asses, someone asked "say end speed"......"75 kts". Obviously not the same reason you are getting at, but still scurry
To my knowledge, there has never been a E-2 or C-2 ditching where everyone lived.
Those gentlemen were awarded Air Medals from CNAF. By all accounts, they should have died on that Cat but were able to save it. I believe the data recorder had them down to 32'. Some good flying they did...
Per AW&ST the F-404 engine (F/A-18C/D) weighs 2,982 lbs, is 154" long & produces 17,700 lbs/thrust in full A/B (5.94X thrust/wt ratio)
The F-414 engine (Super Hornet) weighs 2,445 lbs, is 154"long & produces 22,000 lbs/thrust in full A/B (9.0X thrust/weight ratio)