MOTS Phantom for the RN?

I'm not comfortable with those margins, I could imagine them causing problems exactly when the RN was most vulnerable.
 
So basically COTS Phantoms were not much different in practice on UK carriers than Spey-powered Phantoms with telescoped legs?
 
So basically COTS Phantoms were not much different in practice on UK carriers than Spey-powered Phantoms with telescoped legs?

The longer nose gear delivered, about 12 kts.
From the numbers around, my conclusion is that the Spey made no difference in carrier suitability.

I'm not comfortable with those margins, I could imagine them causing problems exactly when the RN was most vulnerable.

RN would have preferred more and probably expected more from the sales pitch - but went with what the F-4K actually delivered. For the F-4J, the RN would have had to accept that performance from the start.
 
RN would have preferred more and probably expected more from the sales pitch - but went with what the F-4K actually delivered. For the F-4J, the RN would have had to accept that performance from the start.

IIUC then it comes down to timing for a MOTS buy. In 1963-64 the RN was looking at the F4B, which did need the Speys, but when it came time to actually build the aircraft in ~1967 they wanted them based on the F4J which didn't fly until May 1966.

To go with the F4J as a MOTS buy the RN would need to know it was under development early in their process, be comfortable that it would meet their requirements, be confident that it would enter production and that the US would let them buy it. That's a lot of 'ifs' that going with the Spey, that McD themselves proposed in about 1963, would ameliorate. All for the low low price of 25 million pounds development money and some 40% of the aircraft by value would be spent in Britain saving even more precious foreign exchange. Sounds awesome, lets do it!
 
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The F-4K was discussed as a spey-engined F-4J in early 1964, just see the report posted here:



Both options were considered:
1713518445355.png


From this, it is clear that the F-4J with the longer nose gear would have worked from the 199ft catapult, with even the high hopes for the spey showing only marginal improvement; a larger difference was expected with the shorter catapults and slower Hermes:


1713518180475.png

In reality, the spey version fell at least 10 kts/4000lbs short of expectations.
 
Tory Minister Thorneycroft in '62 imposed, McNamara-like, commonality for the Hunter/Sea Vixen replacement. He selected P.1154 18/2/63 (BS.100, 25/3/63), RAF (1-seat) +RN (2-seat).
1/64 (why not 2/63?) he was told 2 engines were vital overwater, VTOL not, so RN 27/2/64 was allowed to escape P.1154B.
He accepted that a MOTS F-4B would arrive sooner/cheaper than an RN-peculiar P.1154, which might also disrupt work on RAF's variant. He authorised R&D for a reheated Spey, but did not then fund $ work, as an Election must soon be held.

New Ministers 27/10/64 funded 4xYF-4K, not fixed price as it was evolving from an F-4B to an F-4J base. They also funded R&D on Spey (to be) 202, though that added (unknown) cost/time. I do not know if jobs led that decision, or if they had been told J79 was incompatible with Ark/Eagle/Victorious - at all, or at tolerable safety. Ministers do not/cannot read graphs, but rely on professionals for techno-input.

CAS knew he had inherited from (now DSACEUR) MRAF Pike a programme that new Ministers would not buy: replacements for Shackleton MR, Beverley/Argosy transports, Canberras, Hunters, plus 5xSSBN, plus...plus...DoD offered US-standard products at fixed Unit prices and on deferred payment terms. Inter-operation with US and other Allies...fixed prices...credit...piles of parts: what's not to like?

Min Defence Healey asked simple Qs on P.1154: on the Central Front, what sortie has VTO+supersonic; in NEAF/FEAF why VTOL at all?
If CAS had said: "so we can operate after AW on our runways"...Ministers might buy no tactical type, and just fund MAD.
If an iron interlude is realistic, runways would be intact, awhile. So RIP P.1154/RAF, 2/2/65. He asked for 175 Long-TOL F-4D/J79, NOW!

The case then made to Ministers was that RN's bolter case required slam reheat, which Spey would do in half a second, as J79 would not, so operationally unsafe. Min of Aviation (Industry sponsor) Jenkins claimed commonality, Spey for F-4M, though RAF did not need it.

(Healey, 13/11/65 revisited £100Mn. saving as J79 now seemed acceptable for RN CVs, but Jenkins carried the Case that canx would do “harm to RR's intnl. standing” A.S.Bennell,Def.Pol.&RAF,P.6.9).

(PM H.Wilson, Memoirs,P.78: Spey: our “well-meant decision proved extremely costly to the taxpayer”).
 
The case then made to Ministers was that RN's bolter case required slam reheat, which Spey would do in half a second, as J79 would not, so operationally unsafe. Min of Aviation (Industry sponsor) Jenkins claimed commonality, Spey for F-4M, though RAF did not need it.

This is sadly funny. Quoting Caygill, "Phantom from the Cockpit":

"...in the case of a bolter, the F-4K taking about 1,000 ft compared with 300 ft for the F-4J."

"Efforts were also made to ... achieve a [Spey] reheat light up time of 1½ seconds (from 3 seconds)."
 
So, an AH would be: no hot Spey for Phantom, MoA Jenkins failing to keep those jobs in UK.
If we take 1965's package as unchanged, then all RR got was dry Spey in Nimrod.

In actual,. next step was BSEL, having lost BOl.320, cuddling up to Pratt/SNECMA on JT9D, 6/66 after abandoning thoughts of a BS.100-aided UK Big Fan. RR had a Demonstrator RB178 contract. Both of them then pitched for Launch Aid to bid to the US TriJets. MoA had a little think about National Interest: BSEL on 747-winning engine, so well placed for a junior role on lots of TriJets, or RR leading a UK Big Fan, pitching v. 1st. mover. (Schemes to be A300 had RB207/JT9D, but volume of business was expected to be modest: BEAC wanted 6).

RR did Ministers' thinking for them and bought 50% of BSEL,10/66, instantly dumping JT9D.

The money to do that came from Spey 202.

So J79/UK: RR unable to buy BSEL. Ministers might well have taken junior on JT9D as a better bet than most of RR, ah, what?

Now take us, via brief AFVG (BSEL/Bristol on M45G) to, 7/68, MRCA, which was won by RB199, offered from ex-BSEL/Bristol.

Ministers Nationalised RR 2/71, when they messed up RB211, ONLY because they had MRCA.

A credible AH is no RR (1971) Ltd, so today no Brit Big Fan.
 
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J79 with overspeed was used by Israelis for Mig25 interception efforts. Ramping up to 18,000lb or more at cost of shorter life.
Did J79 use water injection?

If not overspeed and water injection might solve the problem.

Far out AH is RB.106 Thames instead of Spey. Faster throttle responses from a dedicated fighter engine and 15,000lb dry thrust would overcome a lot of issues.

What do we know of BSEL BS.100 fan engine for transports....?
 
Things are becoming a little clearer on the project decision side.

In 1964 or so McD/USG could give a fixed price on the F4B, but not the F4J as it in development. What's more I think it was pretty much well known that the F4B could not operate effectively even on the 199' BS5A waist cats on Eagle and Ark, even with the long nose oleo and drooping ailerons, or bring back unused ordnance onto their small decks.

So the decision was.
  1. To spend an unknown amount of money controlling development a version of the Phantom that promised launch speeds of 118-129kts @50,000lbs.
  2. To spend an unknown amount of money being a passenger for development of a version of the Phantom that promised launch speeds of 137kts @50,000lbs.
Even in technical terms given the information at the time this is a no brainer.
 
zen #49: BS.123 sampled B.Ol.593 turbine, BS.100 compressor, pitched for MoA' Big Fan Demonstrator, to involve SNECMA.. RR pitched (to be RB178-14, 24,750 lb), evolved from Super-Conway schemes, chosen by MoA 6/65 as the SST was seen as ample BSEL Aid.
 
J79 with overspeed was used by Israelis for Mig25 interception efforts. Ramping up to 18,000lb or more at cost of shorter life.
Did J79 use water injection?

If not overspeed and water injection might solve the problem.

Far out AH is RB.106 Thames instead of Spey. Faster throttle responses from a dedicated fighter engine and 15,000lb dry thrust would overcome a lot of issues.

What do we know of BSEL BS.100 fan engine for transports....?
The F-4Es procured by Israel came with J79-GE-17s - which had a thrust of 11,870 lb dry and 17,900 lb in afterburner.

No, the J79 was not equipped with a water-injection system.

Instead of the Thames, the RR-Allison TF41 could be installed in F-4K/Ms from 1968 on... that "improved Spey" put out 14,500 lb dry in 1968 (USAF A-7Ds) and 15,000 lb in 1969 (USN A-7Es).

Fit a proper afterburner in it and you'll get in the vicinity of 25,000 lb in afterburner (using the same dry:ab ratio as the historic RB168-25 (Mk 201 or 202 Spey).
 
Things are becoming a little clearer on the project decision side.

In 1964 or so McD/USG could give a fixed price on the F4B, but not the F4J as it in development. What's more I think it was pretty much well known that the F4B could not operate effectively even on the 199' BS5A waist cats on Eagle and Ark, even with the long nose oleo and drooping ailerons, or bring back unused ordnance onto their small decks.

So the decision was.
  1. To spend an unknown amount of money controlling development a version of the Phantom that promised launch speeds of 118-129kts @50,000lbs.
  2. To spend an unknown amount of money being a passenger for development of a version of the Phantom that promised launch speeds of 137kts @50,000lbs.
Even in technical terms given the information at the time this is a no brainer.

Yes... with one caveat: The F-4B with the long nose oleo would require around 137 kts @50k lbs, just what the long BS5 + ship speed could deliver.
1713627140808.png
In this sales document, the nrs for the F-4B are always in mil and for the F-4K in AB. Just a subtle nudge.

The J and K would have a better landing performance, but that could be (and was) retrofitted to the F-4B. With the F-4B being lighter, a further advantage...

1713627282759.png
 
What about the bleed air? I've read that the blown flaps in the F4K were more powerful and the Spey provided the extra bleed air for this.
 
What about the bleed air? I've read that the blown flaps in the F4K were more powerful and the Spey provided the extra bleed air for this.
That also caused some challenges for landing. You need high power settings for the bleed air, and if you reduce power you lose bleed air.
 
Does the Spey solve that issue by providing a lot of bleed air at low speeds due to its bigger size?
 
So, an AH would be: no hot Spey for Phantom, MoA Jenkins failing to keep those jobs in UK.
If we take 1965's package as unchanged, then all RR got was dry Spey in Nimrod.
And in Buccaneer S.2.
 
Being derogatory towards Spey powered Phantoms ignores the fact they had superior power in exactly the flight regime for which they spent their mission. I am surprised J79 was adequate because Spey offered so much additional thrust at launch. But maximum takeoff weight and bring back weight dictate operations, not maximum capability.
 
Being derogatory towards Spey powered Phantoms ignores the fact they had superior power in exactly the flight regime for which they spent their mission. I am surprised J79 was adequate because Spey offered so much additional thrust at launch. But maximum takeoff weight and bring back weight dictate operations, not maximum capability.
Again, Spey (and the BLC flaps) greatly complicated the landing due to requiring a high power setting when you're trying to keep a specific speed while descending. And if you cut power, you suddenly lose lift and now you're below the glideslope and RAMPSTRIKE!
 
Surely that can't be unique to the Spey? Surely the J79 had low BLC when landing due to low power settings?
 
Surely that can't be unique to the Spey? Surely the J79 had low BLC when landing due to low power settings?
Yes, for the versions of the F4 that had blown flaps it was an issue, but the US F4s used a lot less blowing overall so it was less visible.

But when trying to land on those postage stamps the RN called Carriers, the F4Ks needed high blowing which meant high power settings.
 
I'm not sure about the advantage of this setting...?

The approach speed of the J and K version was essentially the same in the 1964 McD brochure and in the following F-4K manual (left) and F-4J SAC (right):

1713982216746.png 1713982837086.png


That came out as expected. But on the single engine approach speed, the hope (left) was for 142 kts @ 33k lbs, reality (right) 150 kts - worse than the F-4B, while the 142 kts should be a good guess for the F-4J's single engine approach speed.

1713983096314.png 1713983041755.png
 
With the more powerful blown flaps and the 2 degree greater downward thrust line of the Spey was it more controllable and responsive at the same approach speeds?
 
Hmm.... USN F-4K evaluation and follow-up:
"b) Inadequate throttle control so that it was impossible to set up a stable approach path for carrier operations."

"The obvious need for more thrust to address these problems led Rolls-Royce to look towards reducing BLC bleed air flow...."

"Another concern was uncommanded thrust changes of significant size in the full flap approach configuration."
All Caygill, Peter. Phantom from the Cockpit: Flying the Legend (English Edition) (p.46-49). Pen & Sword Books. Kindle-Version.

Some of that was probably corrected, but improvement over the F-4J, I very much doubt that...
 
Off the shelf Phantoms for the UK should have been bought later rather than earlier.
That way the RAF and Luftwaffe could have operated USAF standard F4Es until the 90s and then collaborated on a replacement.
The RN should have canned its carriers in 1962 in favour of SSGNs.
Lightnings, Hunters, Canberras could all have been replaced by F4Es.
The Vulcans could have been replaced by the cruise missiles developed for the SSGNs.
 
Off the shelf Phantoms for the UK should have been bought later rather than earlier.
That way the RAF and Luftwaffe could have operated USAF standard F4Es until the 90s and then collaborated on a replacement.
The Germans didn't want to shell out for the cash for stock F-4Es and the Brits had requirements that the F-4E couldn't fill, namely the homeland interceptor job (which needed the AWG-10/APG-59 combo) and parts of their overland strike job (FGR.2s got a strike camera and were wired for a recce pod, neither of which stock USAF F-4Es got).

It wasn't going to happen.

The RN should have canned its carriers in 1962 in favour of SSGNs.
SSGNs still can't match the strike capacity of a carrier even today, let alone in the 1960s (before accurate land attack missiles, I might add) and they can't do air defense at all, which is a major problem when Soviet Naval Air is liable to interfere with the ASW job you've so often trumpeted all over the site.
 
The Germans didn't want to shell out for the cash for stock F-4Es and the Brits had requirements that the F-4E couldn't fill, namely the homeland interceptor job (which needed the AWG-10/APG-59 combo) and parts of their overland strike job (FGR.2s got a strike camera and were wired for a recce pod, neither of which stock USAF F-4Es got).

It wasn't going to happen.

Leaving aside the OP being the RAF doesn't need the Phantom; it has made good procurement and fleet management decisions in the late 50s that have paid dividends in the 60s.

SSGNs still can't match the strike capacity of a carrier even today, let alone in the 1960s (before accurate land attack missiles, I might add) and they can't do air defense at all, which is a major problem when Soviet Naval Air is liable to interfere with the ASW job you've so often trumpeted all over the site.

IIRC a RN WW2 designed carrier carried enough ordnance for each aircraft to undertake 4 combat missions. With Ark and Eagle carrying 12 Buccaneers for attack and a basic Buccaneer load being 8 x 1,000lb bombs these ships would be carrying in excess of 350 x 1,000lb bombs. 350 conventional 'warheads' is something a mere handful of modern SSGNs can approach and certainly not possible during the Cold War.
 
I accept your reservations about SSGNs. Save to say there was a lot of vague talk at the time about missiles for the SSNs.

F4s served in the Fighter and Recce roles with the Luftwaffe. I am not persuaded the mods you mention were as drastic as the Spey Phantoms.

An all F4 Luftwaffe and RAFG in the 70s and 80s alongside USAF F4s for much of that time seems reasonable compared with what served.
 
Off the shelf Phantoms for the UK should have been bought later rather than earlier.
That way the RAF and Luftwaffe could have operated USAF standard F4Es until the 90s and then collaborated on a replacement.
The RN should have canned its carriers in 1962 in favour of SSGNs.
Lightnings, Hunters, Canberras could all have been replaced by F4Es.
The Vulcans could have been replaced by the cruise missiles developed for the SSGNs.
"Scrap British, buy American!"

Are you perchance a US sales agent sent forward in time?
 
I was entering into the "off the shelf" theme of the thread. Sadly the F,4 was streets ahead of any UK alternative multi role fighter bomber.
 
I was entering into the "off the shelf" theme of the thread. Sadly the F,4 was streets ahead of any UK alternative multi role fighter bomber.

It's really the only option for the RN, both in terms of capability and cost.

There is no neat trick that makes everything OK for the RN, the only option is for the Government to bite the bullet and spend the money.
 
I accept your reservations about SSGNs. Save to say there was a lot of vague talk at the time about missiles for the SSNs.

F4s served in the Fighter and Recce roles with the Luftwaffe. I am not persuaded the mods you mention were as drastic as the Spey Phantoms.

An all F4 Luftwaffe and RAFG in the 70s and 80s alongside USAF F4s for much of that time seems reasonable compared with what served.
RAF Phantoms had much more stringent air combat capability needs then Luftwaffe Phantoms, given the need to intercept Soviet MPAs and bombers over the North Sea. Look at Foxhunter for what the RAF really thought they needed for the job. APG-59 is a lot closer in capability to Foxhunter than APQ-120.
 
RAF Phantoms had much more stringent air combat capability needs then Luftwaffe Phantoms, given the need to intercept Soviet MPAs and bombers over the North Sea. Look at Foxhunter for what the RAF really thought they needed for the job. APG-59 is a lot closer in capability to Foxhunter than APQ-120.

In this scenario the RAF would have to wait for the ~16 sqns of Lightnings to be replaced by a 4th gen fighter from about 1980 to get this jump in capability.
 
The RN should have canned its carriers in 1962 in favour of SSGNs.
[...]
The Vulcans could have been replaced by the cruise missiles developed for the SSGNs.
Not even close. In 1962, the closest you could get a cruise missile to the target was a CEP of some 1.5 miles/2400m. And, that was using the big warheads that required a missile the size of a Regulus.
 
Guidance was a major hassle. Even with inertial's drift "corrected" by star trackers, CEP still sucked hence big nuclear warheads had to bridge the gap.
 
RAF Phantoms had much more stringent air combat capability needs then Luftwaffe Phantoms, given the need to intercept Soviet MPAs and bombers over the North Sea. Look at Foxhunter for what the RAF really thought they needed for the job. APG-59 is a lot closer in capability to Foxhunter than APQ-120.
Over on the NavWeaps discussion board there used to be a poster using the call-sign Wabpilot.
He was a former USN F-4 & F-14 pilot, and had done an exchange tour on USAF F-4Es in the 1970s.

He assessed the APQ-120 as "slightly worse than the F-4B's original radar in terms of detection target size vs range". Remember that the F-4B's 1961 APQ-72 radar was a slightly uprated larger-antenna (32" dish vs 24") version of the APQ-50 (it was often referred to as "APQ-50(mod)"), which was in the F4D Skyray in 1956.

The USAF's F-4C's APQ-100 (1963) and F-4D's APQ-109 (1965), and the USN/USMC's F-4J's APG-59 (1966) were all much better than the later (1968) small-diameter (because of sharing the nose with the M61 cannon) APQ-120 of the F-4E.

The APQ-120 was first installed in F-4Es in early 1968 - the first 30 F-4Es were delivered without them as it was not ready in late 1967).

The addition of the AWG-10 fire-control system to the F-4S (mid-1970s upgraded F-4Js) made that variant far superior to any other US Phantom (Germany, Turkey, Japan, Korea, Greece, etc all made 1980s & later upgrades that were even better).
 
The relative merits of the F4E vs F4M radars in the British interception context s all well and good in a technical sense but not really relvent because the RAF bought it's Phantoms for use in the fighter-bomber roles after the cancellation of the P1154. The RAF's first Phantom interceptor unit was the F4Ks that were supposed to embark on the HMS Eagle, but were instead diverted to the RAF. The rest of the Phantom fleet didn't become fighters until the Jaguar replaced them in the attack role in the mid 70s, whereby some 6 Lightning sqns were displaced by phantoms in the fighter role, leaving two F6 sqns in service until the late 80s.

This of course is a ridiculous way to provide the RAF with fighter and fighter-bomber capability and exactly what this thread is aimed at avoiding.
 
P1154RAF was an ambitious attempt to provide a Hunter FGA9 replacement for the 70s. It only became ridiculous because of the misguided attempt at commonality with the RN which delayed it for several years.
The planned buy of 150 P1154 would have re-equipped the RAF 38Group, RAFG, Air ForceGulf and FEAF Hunter squadrons.
Faced with delays and costs the cancellation was unavoidable and the RAF received F4s and P1127Harriers by 1970 (P1154 could not have reached service so quickly).
The RAF then turned the Jaguar trainer into a replacement for P1154 allowing the F4s to replace most of the Lightning force. As the RAF had needed a Lightning replacement this was reasonable.
I only suggested an F4E force to replace this process to match what the Luftwaffe wanted (it was not keen on MRCA) and am quite happy with what the RAF did. I would like to have seen P1154RAF work though
 
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