Let’s face it, LM/KAI’s T-50 is a mini F-16, in other words a 4th gen jet. Who want’s to train 5th, 6th, possibly 7th gen fighter pilots in an F-16?
As opposed to a derated, fattened Gripen offspring?
The USAF seems to have successfully trained F-22 pilots using 1950s-designed T-38s. The Italians and Israelis have F-35 pilots coming up through the M-346, which by your reasoning must be impossible since it failed T-X.
It has nothing to do with ‘generations’ of trainers, all that fancy stuff is done in the simulator. A T-X of any type can’t emulate an F-22’s TVC, or an F-35’s sensor fusion.
Diplomatic row with US jeopardizes $1.5 billion deal between Turkey and Pakistan
Well yes, “never fit a US engine to your indigenous airframe” has been known about since Sweden hit the problem in the mid-1930s. And yet 80 years later the Turks are making the same mistake. Who’s the foolish one?
And in a similar vein, Martin AM-1 Mauler:
Still deadly 33 years after that attack against HMS Sheffield…
Can’t really give any credit to the Super Etendard for that, though. The Iraqis had a better idea when they strapped a pair of Exocets to a Falcon 50. Longer range, shirt-sleeve cabin, toilet and galley.
The Argentinians might have been more potent had they converted their Neptunes or Electras to carry Exocets. They could have ranged well out into the Atlantic.
On 15 May two T-6C Texan IIs for the RAF made a stopover at Glasgow Airport. The aircraft will be delivered to RAF Valley.
I’m still not clear why they chose a warmed-over 34-year-old design in preference to the PC-21. Just look at all those aerodynamic bodges. Of course, commonality with the USA.
At least QinetiQ have chosen the PC-21 for the ETPS. A design that has some potential for the future instead of being at the limits of its airframe.
Wonder if there is any particular reason why all the airworthy -1 Corsairs are Goodyear built airframes?
Many of the 1945 Goodyear-built airframes didn’t see wartime service. It would be interesting to map the airworthy FG-1Ds to their production dates.
Edit:
2 FG-1D (N700G) 1944
3 FG-1D (N773RD) 1944
4 FG-1D (N11Y) ?
5 FG-1D (N83JC) 1943
6 FG-1D (N46RL) 1945
7 FG-1D (N72NW) 1944
8 FG-1D (C-GVWC) 1945
9 FG-1D (N29VF) 1945
10 FG-1D (G-FGID) 1945
11 FG-1D (ZK-COR) ?
12 FG-1D (N43FG) 1945
13 FG-1D (N209TW) 1945
14 FG-1D (N451FG) 1945
15 FG-1D (N9964Z) 1943
Here’s an interesting video; tactical weapons effect trials by USAF in 1963
https://youtu.be/ig4XOziHC2Q?t=795
They mounted a camera on one target to capture a view of the 2.75 FFARs inbound from that F-100D
They went with the F-16 because the US pressured them to, the original FS-X was an F-18 looking aircraft with canards
The F-15, F-16, F-18 and Tornado were all proposed alongside the indigenous design either as straight purchase or redesign.
There was huge pressure to choose US, of course, but the F-18 was actually pushed harder than the F-16. But the Japanese felt that the F-16 was the cheapest and lowest-risk as a basis for redesign.
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In theory yes the ADV could carry anything the IDS could except JP233 and MW-1, but in practice it was only cleared with the usual AAMs.
With a much better fuselage fineness-ratio it had the aerodynamics that the IDS lacked, and so a similar stretch was proposed for the Tornado IDS 2000 upgrade.
Needed more thrust and more area-ruling to meet its potential. Should have had a pair of Helwan E300s. Later the RB.199 and Atar 9K50 were both studied for the single-engine Marut Mk 3 but didn’t proceeed.
Also usually flew with two of the 30mm cannon removed due to vibration issues when firing.
Japan had another look at the F-15 in the mid-1980s as a basis for FS-X but went with the F-16 purely on cost grounds. Other than price the only practical downside they identified for the F-15 was its lack of stealth potential ( yes they used that term even in 1985 ) and since the F-16 met the requirements and was also non-stealthy they went with the smaller airframe.
I imagine I’m typical of most kids growing up in the UK during the Cold War in wishing that the RAF had F15s instead of Tornado F3s, but with a bit of distance and reflection it wasn’t a terrible decision.
Well the main reason for selecting the ADV was cost; to keep the per-unit Tornado costs in line the UK had to meet its original target of 385 airframes. As early as 1976 the ADV was being described as ‘satisfactory’ for the role envisaged which was faint praise. An F-15B with UK radar and systems would probably have been better in every way except cost.
Also around the same time AST.403 requirement emerged for a tactical high-agility successor to Jaguar and Harrier, for which the F-16 was pencilled-in. So the lack of dogfighting capability in the ADV wasn’t seen as critical as it wouldn’t be mixing with MiGs.
Fomr the Flight archive, 1976 airframe prices listed by the UK MoD in response to Parliament queries: F-14 £10 million, F-15 £7 million, ADV £6.5 million projected. Plus additional costs for the US options in fitting UK equipment and increase in unit costs for the 220 IDS on order.
So, what about the stories of Bears out-accelerating ADV’s?
In dry-thrust, yes. Rather embarrassing but the RB.199 was wheasy at altitude, as noted earlier. But bring in partial reheat and all that lovely bypass air gave a good kick. The ADV could also chase-down nearly anything at sea-level, rumoured to include F-111s.
Also I noticed whilst browsing books today that the outer hardpoints of the ADV were plumbed, and with pylons installed could in theory carry another pair of Hindenburg tanks. Or an AMRAAM each, or triple-clusters of ASRAAM!
The Japanese FS-X ADV would have had the outer wing points activated for IR AAMs, plus antishipping missiles inboard. I can’t remember if it was to retain the fuselage MRAAM recesses; II think it did as I recall a model with 10 or 12 AAMs which in the pre-Flanker days seemed incredible.
The late-80s were bleak for Panavia; Italy had stopped at 100 ( declined a batch of 30 more ), the Jordanian and Turkish orders fell through and the USAFE decided against the ECR Wild Weasel.
Gee are we still going around this roundabout of irrelevance.
No-one is going to pick an MPA platform on the basis of potential emergency performance. Frankly none of the bean-counters that make the decision give a toss about such a narrow, rare scenario. It’s all based on mission-capability, lifecycle cost and politics.
The first time around in the 1980s Boeing picked the 757 as its platform for the LRAACA requirement. By the late 2000s that was no longer an option so they chose the 737NG as the next best platform. Not because it could do a barrel-roll on one engine or could out-turn an SA-12, but because it was available, efficient and a 767 was too big. That’s all!