GreenKnight121
Senior Airman
- 732
- Mar 16, 2014
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I aways liked the look of the wing top missiles on the Sepcat Jaguar.
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The over-wing pylons also are useful for system pods.
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The Jaguar is one of my favourite aircraft of the 1980s. With its arrestor hook, good short runway capabilities, twin 30mm cannons and Martel antiship missiles, a squadron or two would have done nicely pre-war at the Falkland's.
I bet Ukraine could do wonders with the Jaguar even today.
Describe the Jaguar in three words
"Comfortable, ergonomic, underpowered.
Complete this sentence: The Jaguar needed…
"More development in all areas."
What was the best thing about the Jaguar?
"Relative ease of day visual single seat operation at low level (LL)."
..and the worst?
"Lack of thrust."
Take-off/landing performance
"Landing first, easy, precise (⍺), brake parachute equipped with big brakes – excellent! Take-off has been variously described as due to the curvature of the earth and was certainly an Operations Manual reference event depending on entropy, configuration and airfield. Reliance on 'clear wing' after engine failure would be operationally standard. Full reheat was standard and operational formation take-offs would be a race to the first waypoint."
Did it have enough power?
"There was never enough power and the Adour, an Anglo/French cooperation, was optimised for high take-off thrust in reheat, good specific fuel consumption, providing a high speed dash capability and was to be changeable in 30 minutes! Good job there were two. Engine improvement were forthcoming including 'part throttle reheat' (PTR) to improve single engine handling, arguably also survivability, allowing reheat at less than maximum engine N1 rpm. Eventual Adour marks improved all engine performance aspects but there was rarely spare power, depending on the configuration."
Climb rate
"Totally weight and configuration dependent but the clean aircraft at 10 tonnes had a T/W of 0.5 similar to a Hawker Hunter, and climbed to 30,000ft in just over 1 minute. Fully war configured time to height was fairly pitiful and very fuel consuming."
Given Peter Day's experience as detailed it is unlikely that he experienced the 2 engine upgrades that were implemented during life of the Jaguar. In the 1970s the engine was the Adour 102 - 5,110lb dry & 7,300lb with reheat.Missed the bolded part before... it definitely tripped an alarm this time.
First I've heard of this... the normal comment I've heard about the Jaguar's runway performance is along the lines of "Jaguar takes off by the earth curving away below it".
Here is an interview with a former RAF Jaguar pilot (Peter Day*): I flew the Cold War Jaguar fighter-bomber
He gives a slightly differently-worded but essentially identical comment as mine above:
* Peter Day's resume:
Jaguar Conversion Unit (226 OCU) Jun – Sep 1974
No 6 Sqn RAF Coltishall Oct 1974 – Apr 1977 'Flying Can-openers'
No 14 Sqn RAF Bruggen May 1977 – Aug 1980 'Crusaders'
HQ RAFG Jaguar Staff Officer Sep 1980 – Feb 1983
1500+ flight hours Jaguar
So take off performance would depend on when the pilot making the claim was flying them.
Good info, and well cancels my idea for Jaguars at pre-war Stanley. I should have surmised that the Jaguar needed a lot of runway when at 2:20 they faded to black during a non-takeoff takeoff vid.First I've heard of this... the normal comment I've heard about the Jaguar's runway performance is along the lines of "Jaguar takes off by the earth curving away below it".
It's noteworthy that in the post-war era that aircraft designers omitted to include sufficient internal fuel load in almost every aircraft, and that engine designers could not provide sufficient fuel efficiency to permit allowance on internal fuel. Is there any Cold War supersonic fighter that could make do without external fuel tanks? The Lightning looks ridiculous with its over-wing tanks, but at least they're not occupying otherwise useful underwing pylons. Look at this F-15 below, now that's what wing pylons are for!A funny anecdote I heard from an RAF bod once was that the Jaguar was the only RAF aircraft in which its take-off run was counted as a part of its combat radius...
One reason for the Jag's overwing pylons was because the inboard wing pylons were almost always occupied by fuel tanks, thus leaving only two wing pylons and a centreline one for armament.
It's noteworthy that in the post-war era that aircraft designers omitted to include sufficient internal fuel load in almost every aircraft, and that engine designers could not provide sufficient fuel efficiency to permit allowance on internal fuel. Is there any Cold War supersonic fighter that could make do without external fuel tanks? The Lightning looks ridiculous with its over-wing tanks, but at least they're not occupying otherwise useful underwing pylons. Look at this F-15 below, now that's what wing pylons are for!
View attachment 774116
Whatever range you design an aircraft to reach, I can guarantee you that there will always be a mission profile that requires longer range.
With carrier borne aircraft the position of the carriers depends on the aircraft's range, which would rarely be enough for the captain of the carrier.Whatever range you design an aircraft to reach, I can guarantee you that there will always be a mission profile that requires longer range.
True. But it does spoil the looks of a F-22 of F-35 to swing a pair or trio of drop tanks under the wings. I think somehow their designers sorted out how to conduct most missions on internal fuel, with AAR as needed. Perhaps supercruise helps. Do external tanks like the below impact the stealth capabilities?Whatever range you design an aircraft to reach, I can guarantee you that there will always be a mission profile that requires longer range.
Ever since the F-15C/D entered service the aircraft have been configured to carry the Conformal Fuel Tanks as shown in your photo. These are non-jettisonable which may or may not be an advantage. The slab sided engine intakes on the F-15 make it easier to design in but it has been done to others.
It's noteworthy that in the post-war era that aircraft designers omitted to include sufficient internal fuel load in almost every aircraft, and that engine designers could not provide sufficient fuel efficiency to permit allowance on internal fuel. Is there any Cold War supersonic fighter that could make do without external fuel tanks? The Lightning looks ridiculous with its over-wing tanks, but at least they're not occupying otherwise useful underwing pylons. Look at this F-15 below, now that's what wing pylons are for!
View attachment 774116
CFT were previously known as FAST (Fuel and Sensor Tactical) packs. Developed in the early 1970s and first flown on an F-15B in 1974. The first F-15C flew in Feb 1979 and all production F-15C/D were equipped to carry them and did so from the introduction of those models in June 1980. 32nd TFS at Soesterberg in the Netherlands was the first to get the updated model.Small niggle: the conformal tanks were introduced with the -E model Strike Eagle, though they can be mounted on earlier models.
PerhapsBiffF15 could comment on the relative flight qualities?
CFT were previously known as FAST (Fuel and Sensor Tactical) packs. Developed in the early 1970s and first flown on an F-15B in 1974. The first F-15C flew in Feb 1979 and all production F-15C/D were equipped to carry them and did so from the introduction of those models in June 1980. 32nd TFS at Soesterberg in the Netherlands was the first to get the updated model.
The F-15E development started as a privately funded development in the late 1970s with a demonstrator first flying in July 1980 and the first production aircraft in 1986.
Thump,Small niggle: the conformal tanks were introduced with the -E model Strike Eagle, though they can be mounted on earlier models.
PerhapsBiffF15 could comment on the relative flight qualities?
Thump,
Smaller niggle, the CFTs (Conformal Fuel Tanks) were introduced on and delivered with every F-15C/D bought by the USAF.
Photoshop
Photoshop
True. But it does spoil the looks of a F-22 of F-35 to swing a pair or trio of drop tanks under the wings. I think somehow their designers sorted out how to conduct most missions on internal fuel, with AAR as needed. Perhaps supercruise helps. Do external tanks like the below impact the stealth capabilities?
View attachment 774120
It's noteworthy that in the post-war era that aircraft designers omitted to include sufficient internal fuel load in almost every aircraft, and that engine designers could not provide sufficient fuel efficiency to permit allowance on internal fuel. Is there any Cold War supersonic fighter that could make do without external fuel tanks? The Lightning looks ridiculous with its over-wing tanks, but at least they're not occupying otherwise useful underwing pylons.