Aviation installations in Audacious, Clemenceau and Essex Class: Catapults, Arrestor Gear, etc...

orlovsky

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I guess this is the right place - "historic... ships... not unbuilt projects".

I have a certain fascination with that old massive “analogue” technology: Audacious class, Clemenceau class, Essex class. The RN made Ark Royal fly Phantoms, the USN put large air wings on the Essexes, and the Clems look used way below potential, especially with the Crusaders finding no replacement.

The informations on the key aviation installations are piecemeal and murky. I will start with the steam catapults, especially on the Clemenceau class, in this first post.

Some interesting articles can be found in the JNE online:

The steam catapult (1953) https://library.imarest.org/record/10138?ln=en&p=steam+catapult

A steam catapult installation (1957) https://library.imarest.org/record/9939/files/v10b2p07a.pdf

Flight deck machinery (1965) https://library.imarest.org/record/9395/files/v18b1p08a.pdf

Development of the steam catapult (1966) https://library.imarest.org/record/9505/files/v16b3p04a.pdf

The catapults used were british BS4, BS5 and C-11 and the derived American C-11-1, being a rather close family. The end speeds for 1950s/60s fighter weights are:

33k lbs: short BS5 108?, long BS5 123?, C-11-1 133-137
40k lbs: short BS5 101, long BS5 116, C-11-1 125-129
44k lbs: short BS5 97, long BS5 111, C-11-1 120-126
50k lbs: short BS5 91, long BS5 105, C-11-1 115-120

BS5 details here, subtract 28 kts shipspeed and 4 kts engine.
1776456865581.png

Within the family, the differences are accounted for by about 0.3 kt per ft stroke length, and between the BS and C series additionally about 10 kts for difference in steam pressure.

As discussed several times, the nrs for the BS catapults in the Clems do not really fit. Actually, they are all over the place.

From French material around 1960 for the 157 ft catapults:
1776456883137.png

Despite the higher steam pressure and similar length, the end speeds align with the short RN BS5.

First edition (1980s) of Moulin's book on Clemenceau and Foch states a more powerful 51,5m (169 ft) bs5 with 110 kts @ 20 metric t replaced a bs4 with 95 kts @ 20t, 110 kts @ 15t and 130 kts @11t. He does not say when this happened, but the new figure would be 15 kts above the short RN BS5: ~5kts from length, ~10 kts from steam pressure. Makes sense.

1776456903785.png

This would also fit with the requirements for the F-8 operating smoothly and no big problems seen for the F-18. With the original numbers, both would be extremely marginal to impossible.

Unfortunately, the 2006 edition of Moulin found that the catapults had not been changed. Rather, there was a small change in the BS4, the RN decided to rename the later versions as BS5, and the MN followed.
(The author adds “...to avoid any confusion”, and in a footnote “Obviously, that did not turn out so well” – someone was not happy). Moulin then has figures for end speeds that look inconsistent and do not mention the timeframe or whether they are for maximum or mean g load. No mention of an improved version, 20t/44k lbs are suddenly just at 90 kts.

But as said, the original numbers have likely been improved for the F-8 and for consideration of the F-18. Moulin has the catapults at 51.5m (169 ft), so at least lengthened by the typical 12 ft increment. Should be worth 3-4 kts. Also, that on Foch the steam pressure was increased to 570 psi from 550 – probably a very small improvement.

The french material from ~1960 also mentions a perspective: Changing from dry to wet accumulators, studied by the RN and foreseen as a change of the accumulators in RN carriers:
1776456937147.png

I had not seen any information on results from this, just numbers for the C-11 “dry” and “wet” with very little difference. But on the RN BS5, it was applied with substantial result by the early 1960s (DEVELOPMENT OF THE STEAM CATAPULT, cf above):
1776456962256.png
1776456981115.png

I consider it very likely that this has also been applied to the French BS5: The MN was aware of the development, it was needed for the Crusaders and it looks like a relatively simple change. At 44k lbs, this would give from the basic 95 kts +3-4 added length +8-10 wet accululators, and we are in the 105-110 kt range as mentioned in the initial edition of Moulin.

Only problem: I have not found confirmation that the accumulators on Clemenceau and Foch have been changed. It might be an issue too arcane even for specialized authors like Moulin (who initially fell victim to the BS5 renaming…)
 
For arrestor gear:

From Flight deck machinery (1965) https://library.imarest.org/record/9395/files/v18b1p08a.pdf

The Mk 13 arresting gear was "installed in all [RN] fixed-wing carriers" as well as the Clemenceau class.

"This gear came into service in 1955 in H.M.S. Ark Royal with a performance of: up to 110 kts at 20,000 Ib up to 105 kts at 30,000 lb"

"The gear was uprated in 1960 to a performance of up to 112 kts at all weights up to 30,000 lb and at speeds equivalent to an energy of 16.7 X 10^6 ft lb at weights from 30,000-37,000 lb."

"A further uprating t o a performance of 120 kts at all weights up to 30,000 Ib and at speeds equivalent to an energy of 19.2
X 10^6 ft lb at weights from 30,000-40,000 lb has been agreed and is being released to the Fleet. The latest increase in performance has been obtained without modification to the arresting gear and is based on accumulated in-service and trials experience, and a recently acquired ability to measure aircraft entry-speed." (1965)

So until 1960: up to 20k lbs @ 110 kts, 30k lbs @ 105 kts.
1960-65: up to 30k lbs @ 112 kts, 37k lbs @ 101 kts calculated from energy
1965- : up to 30k lbs @ 120 kts, 40k lbs @104 kts calculated from energy
Moulin (2006) has 40k lbs @112kts for the Clems (while deck strength limit 33k lbs) which would be a further improvement.

Essex class CVAs used the mk7 mod 1:

1778056699780.png

So up to 20k lbs @ 130 kts, 25k lbs ~125 kts, 30k lbs ~ 120 kts, 40k lbs @115 kts. I have not seen anything about earlier more limited versions.

This Mk7 has a varying advantage over the Mk13. Explains why the landing speed of the F-8E(FN) was such a crucial point for the french carriers: 1962/63 we'd have 112 kts from the british Mk13 vs 125-130 kts from the american Mk7.
Also for the original F-4B we'd get 140 kts approach speed vs ~105 kts gear limit 1960-65, so this would have been a bigger problem than the catapult limits for an Aeronavale Phantom (ignoring the financial problem). With the later reduction in approach speed and the uprating of the gear it looks workable, though.

And the RN with an eye on the phantom (?) started work on the dax2/mk14 gear in 1962...
 
Jet blast deflectors:
Oriskany and co had a Mk3 deflector, would have to be replaced by Mk7 for F-18. From the estimate here, JBDs were a very minor source of costs.

1779024511987.png

From the USN training books, the Mk3 was already water-cooled. Differences of size and raising method, probably.
1779025407668.png

Ark Royal got a unique V-shaped JBD for the F-4K in the phantom refit 1967/70. Not much information about the earlier model used.

New to me, from Moulin 2006, p 177, Clemenceau and Foch received new JBDs for the Crusaders. Water-cooled and made by Breguet, but still comparatively small. Original were models by Mac Taggart, probably the same as on RN carriers with the exception of the phantomized Ark.
 
For the catapult question on the Clems, I hoped to find some information whether they switched to wet accumulators or for other changes like in the valves. No success, but on the last pages of this thread https://www.anciens-cols-bleus.net/t7123-foch-pa-tome-1 there are some on-board booklets from Foch that confirm the improved performance: 33k lbs @ 130 kts, 44k lbs @ 108/110 kts:

1779026900111.png
1779026952403.png

The data in Moulin 2006 is a bit confusing, but he has examples of varying weight/g/endspeeds, which are not the maximum. This is clear from the text itself. For example:
Mass (mt) / Speed (kn) / Acceleration (g)
10..................115.................4.0
10..................105.................3.3
15..................105.................3.5
20....................90.................2.8
Just above the table, he states that a SuE at 10.7 tons would be launched with 122 kts endspeed and 26.6 bar steam pressure (with the maximum being 38.7 or 40). With full steam pressure it would probably be 140+ kts.
 
Well, it's all relative. The shipyard manday rate back then was 200-300$, so this gives an extra ~2 million $. Compared to the total Oriskany reactivation cost or a Forrestal class SLEP of 500 million $ it is a very minor cost.
 
Well, it's all relative. The shipyard manday rate back then was 200-300$, so this gives an extra ~2 million $. Compared to the total Oriskany reactivation cost or a Forrestal class SLEP of 500 million $ it is a very minor cost.
My WTF was more in terms of scope of that single piece of work to do, for what should be a pretty simple thing.
 

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