First flight in 1966, so not completely hopeless."Look down / shoot down" through pulse-doppler came with the AWG-10 and F-4J.
Saying that kpuscas, the F-100's offensive punch was still somewhat limited in terms of bomb/rocket/missile load in my opinion- especially when one considers, by all accounts (using pictures from Vietnam War), that two of it's hardpoints were almost always required for drop tanks and bombs and rockets were seemingly of single pylon arrangement vs multiple pylons used by other USAF aircraft.You could argue the last "tactical" focused aircraft the USAF bought was the F-100.
Yes, that would be very nice. And if the wingtip pylons could also take the weight of a Y rack and 2x Sidewinders, that'd give you 8x total, plus all 3 drop tanks. Or 10-12x if you put the Y ranks on all 4 underwing pylons, drop tank on centerline. 10x Sidewinders if you have single mounts on the wingtips, 12x if you can get Y racks to work there.
If they don't have an AWACS to help guide them in, they're going to need better than a gun-ranging radar.
And that gets into it. The USAF did take lightly armed F5As up over north Vietnam (dragging them via inflight refueling) but didn't have any encounters with MiGs.
Probably equal to a MiG17 as-is, adding modern radar guns and sidewinders would be a lot of money.And the F-86 ? Could it have been an effective fighter against the MiG-17s ?
ANG F-86H.
Or perhaps a version of the F-86K with modern radar, cannons and advanced sidewinders.
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FJ-4s should do nicely.
Their J65-W-16A engines were more powerful than most J47s (their 7,700 lb thrust matched the afterburning J47s of the F-86D/Ks), and they were designed for higher-altitude fighting than the F-86s were... they could engage in combat up to 49,000 feet - higher than even the F-86Fs could.
Their level-flight max speed was .95 Mach, and they went trans-sonic in a slight dive easily and just past Mach 1 in a moderate dive.
They carried more internal fuel than any other F-86/FJ model did (50% more than the FJ-3 or F-86E), and carried 4 AIM-9s rather than the 2 of the F-86s. They also had a decent radar-ranging gunsight - all they would need is someone to tell them where to look.
It shouldn't be too hard to fit the 8,400 lb J65-W-20 (used in the A-4Cs and retrofitted to A-4Bs) or upgrade their -16As to -20 standard if necessary - this would really boost climb and help sustain maneuver energy.
150 had been made for the USMC, all of which were retired by 1965 (even those in reserve squadrons), so they would be available.
Those were the 222 FJ-4B ground attack/tactical nuclear weapon delivery versions... the 150 FJ-4s were straight fighters only issued to 3 USMC squadrons and one USN training squadron.I thought they remained in service with the Naval Reserve until the late 60s.
Read somewhere that the M53 performs better than the F100 (at least the early ones) at high altitude/speed for this reason. Same with the TF30/F110 in the Tomcat.** All turbine engines lose some thrust at high altitudes, but turbojets lose a smaller percentage than do turbofans. This places a turbofan at a disadvantage when trying to reach high speed at high altitude when compared to a turbojet of equal sea-level thrust output. The Spey produced more sea-level thrust than the J79 - but as the aircraft neared its combat ceiling its thrust actually dropped below that of the J79.
Oh? That would be just about ideal for the lower end (MiG15/17/19) but would definitely struggle versus the MiG21s.The RAAF had a small sqn of Avon Sabres based at Ubon in Thailand 1962-68, armed with 30mm cannon and Aim9b. They indirectly supported the US effort by defending Ubon, but restrictive RoE saw them sidelined and their sorties bumped for USAF Rolling Thunder sorties. I'm sure if the situation arose they'd give a good account of themselves, but to think they'd be as good as new and more capable planes is wishful thinking.
Indeed the Commonwealth Aircraft Corporation-built aircraft were the best of the non-naval Sabre type - their Avon RA.7 engines put out 7,500 lb of thrust, so they also had trans-sonic capability. Their two 30mm Aden cannon were good (if a bit limited by 162 rounds per gun), but they were only fitted for 2 AIM-9 missiles - an improvement to 4 would have been necessary.Oh? That would be just about ideal for the lower end (MiG15/17/19) but would definitely struggle versus the MiG21s.
Avon Sabres were the best of the type.
Sorry Archibald, but I would think the J79 would be too big and heavy for the F-5/F-20 design in general.....Which might bring us back to a N-102 Fang derivative, incorporating the learnt and built lessons of the F-5.....?How about a "proto F-20" that is a F-5E with a J79 ?
The RAAF had a small sqn of Avon Sabres based at Ubon in Thailand 1962-68, armed with 30mm cannon and Aim9b. They indirectly supported the US effort by defending Ubon, but restrictive RoE saw them sidelined and their sorties bumped for USAF Rolling Thunder sorties. I'm sure if the situation arose they'd give a good account of themselves, but to think they'd be as good as new and more capable planes is wishful thinking.
In addition to the Sabres in Thailand the RAAF deployed a small sqn of Canberras in Sth Vietnam from 1967. One was shot down by a North Vietnam SAM.
Mirage IIIO were deployed to Butterworth Malaysia in 1968.
Its not beyond the realms of possibility that RAAF Sabres or Mirages might see combat against NthV fighters with some different government or RAAF decisions.
IIRC the Sabers had 2x pylons per wing, so wiring and adding the Argon bottles should be relatively simple.Indeed the Commonwealth Aircraft Corporation-built aircraft were the best of the non-naval Sabre type - their Avon RA.7 engines put out 7,500 lb of thrust, so they also had trans-sonic capability. Their two 30mm Aden cannon were good (if a bit limited by 162 rounds per gun), but they were only fitted for 2 AIM-9 missiles - an improvement to 4 would have been necessary.
The .50cals would be basically useless. It takes way too much .50cal fire into an airplane to break something flight-critical.The Canadair Sabre Mk 6 was almost as good as the Australian Sabre... the Orenda 14 engine put out 7,275 lb thrust (and bumped the service ceiling from the 48,000 feet of the F-86F to 55,000 feet) - but the retention of the 6x.50MG and lack of AIM-9 capability were a negative.
They were, however, available (having just been replaced by F-104s) and wiring them for AIM-9s would not be a problem.
I would take an F-4 over two F-5 over Vietnam every time. The F-4 is truly useful for multirole but the F-5 barely covers a few minor niches. People forget in those days there was no such thing as a multipurpose aircraft.
IIRC the Sabers had 2x pylons per wing, so wiring and adding the Argon bottles should be relatively simple.
As to the guns, if the pilot can get a hit with a burst of 10-20 rounds per gun, a single 30mm will do ugly things to a plane.
The .50cals would be basically useless. It takes way too much .50cal fire into an airplane to break something flight-critical.
I like the Lockheed Lancer. It's what the F-104 should have beenUpon further research my proposed wing isn't even necessary.. I still like it for obviously flawed and biased reasons.. But the 98-L version of the Tiger/SuperTiger or the F-12 with 350 sqft. wing that developed out of it would be totally fine for the job! The Air Force evaluated the supeTiger and gave it excellent reviews inclusive of the test team recommending it for purchase.
You can get close to the 98-L by swapping the wing tips with slightly larger ones to bring the span to 34 feet from 31 and change.
They would be facing Korean War era fighters for the most part. MiG17s. This is basically applying Boyd's Fighter Mafia thinking at about the time he was developing the idea: Yes, you have the expensive highly capable planes (F4s for Vietnam), but those don't give you the mass numbers you need. So you pull some relatively capable aircraft out of the Boneyard, like FJ-4s.Sounds like you don't care about true Air Superiority. Korean War era fighters, even with a bigger engine and more fuel, have little room for improvements. The lesson over Vietnam is never get complacent. What was superior early wasn't so hot for long. The platform has to evolve. And by the way, budgets matter so you want to stick to fewer platforms for more roles. Change the equipment and aircrew but use the same plane. The F-4 was the poster child of this strategy.
And the F-5 for a short time.By my count the USAF tried 4 fighters in Vietnam; F100, F102, F104 and F4, they didn't use the F101, F106 or re-activate older designs even though they could have if that was the best way to go.
Probably. Which would have required seeing that the USAF training was deficient in WVR encounters in about 1960, maybe 1963 at the latest if you are trying to get a plane into service in 1968.That suggests that of the aircraft immediately available to it the F4 was the best aircraft for the job. I think the only way to beat the F4 would be a clean sheet design.
The F8U was not more maneuverable. The F5D had better TW and WL, much higher climb rate, better visibility, and longer range. The only advantage the F8U has is its speed.F5D was limited by wave drag. I see no reason it was superior to F-8 in the stock engine let alone if F-8 had been equipped with J79. They both shared the same radar and F-8 just needed the director equipment for Sparrow to match F5D. The F-8 was superior in agility, mobility, and raw speed; keys for survival in that age. F5D offered nothing over that save for potential to be a larger target.
I suggested the crossbreeding to create a joint design between two companies that equipped both services. The two eventually would merge.
Baloney. The F-8 had better roll rate, instant turn rate, and sustained turn rate. And its better speed and accelleration is because of its less draggy design. And F5D had lower TWR. F-8 clearly was the superior energy fighter. F5D never ever had J79. This constant rewriting history that F5D is magical once it gets J79 is bothersome because F-8 would have just as readily had the same engine upgrade path available.The F8U was not more maneuverable. The F5D had better TW and WL, much higher climb rate, better visibility, and longer range. The only advantage the F8U has is its speed.
...The F8U was not more maneuverable. The F5D had better TW and WL, much higher climb rate, better visibility, and longer range. The only advantage the F8U has is its speed.
And the F-5 for a short time.
Probably. Which would have required seeing that the USAF training was deficient in WVR encounters in about 1960, maybe 1963 at the latest if you are trying to get a plane into service in 1968.