There will be NO Sea Typhoon, page 2
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reply posted on 10-12-2008 @ 07:20 AM by stratsys-sws
reply to post by RichardPrice



I'm with Richard on this one, the idea that an aircraft "looks" less sturdy is nonsense. The undercarriage design on the EF2000 is much more recent than any of the aircraft previously mentioned, design and material improvements may mean an equal specification may be much lighter than an older model. Positioning of the gear doesn't really have much bearing either (pardon the pun)

However, having said that...The undercarriage would need to be upgraded! The Typhoon was not designed for carrier ops, the undercarriage is designed for the lighter requirement of conventional landings, thus saving weight.

The major considerations in a navalised Typhoon would be

1. High Alpha required at the slow speeds needed for carrier landings obscuring pilots view, potentially made worse by the canards

2. Undercarriage Specification

3. Deck clearance of weapons

4. Deck Mounting Points/access

5. Anti-Corrosion coatings required in high moisture/salt environment

6. Re-certification of pretty much every component for carrier ops!

I agree that a navalised Typhoon would pretty much need to be designed from the ground up.

Cheers

Robbie


reply posted on 11-12-2008 @ 04:14 AM by Fang
reply to post by solidshot


On current projections this places the delivery of the Carriers in sync with that of the JSF.

It's not about cutting costs but spreading them over a longer accounting period.


[edit on 07/21/06 by Fang]


reply posted on 15-1-2009 @ 09:53 AM by Harlequin
reply to post by CloudySkye



General Sir Kevin O'Donoghue is the man who signs the cheques - so if he says `no` it doesn`t matter if the aircraft can and can`t do it - it won`t happen.


and remember this is BAe Systems so what ever happens it`ll be over budget and way over time.


*cough* MR4a *cough*


reply posted on 16-1-2009 @ 01:54 AM by Daedalus3
Originally posted by RichardPrice
Originally posted by stratsys-sws

1. High Alpha required at the slow speeds needed for carrier landings obscuring pilots view, potentially made worse by the canards



Never been an issue before - procedures have been in place for many years to minimise the effect of lower visibility on carrier approach.



True.. The Rafale seems to do ok with canards on the carrier deck. Also the supposed J-10 would have the same hurdle to overcome; if it was a hurdle. The nose down, cockpit forward concept should compensate for any of this I think.


As noted previously, the current Eurofighter is specced to rough field level, so it wouldn't require as much upgrading as expected.


That might be a problem. The considerations for naval catapult launched and arrester recovery u/c are immense. Not to mention the High rate of descent + High AoA landings; but then again, nothing a normal a/c carrier conversion program wouldn't handle. Its been done to numerous a/c over the ages and the UK has more than enough experience + expertise to work this out.


3. Deck clearance of weapons
....
The center pylon has more clearance than the F/A-18 does, while the rest of the pylons are forward of the main gear.


Interesting point.. I have heard of technical complications when IN Harriers would fly with Sea Eagle AS missiles on wing pylons (center pylon not an option). Conducting a vertical landing with only one missile on either wing was apparently a nightmare. I can't recollect where I heard this. Any similar experiences in the RN etc?


5. Anti-Corrosion coatings required in high moisture/salt environment
....
The Eurofighter is built to export standard, meaning all parts are already certificated to the standard required.


Standard conversion process. Like I said, done to many an a/c, so its not rocket science.
Carrier conversion is not a big deal. Definitely cheaper in teh longer run when compared to setting up logistics and infra for a completely new a/c.
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