A listing of Blue Jay variants and derivatives, including info from Tony Wilson's English Electric Lightning Genesis & Projects.
Blue Jay Mk.1 – stern-chase IR-guided, entered service as Firestreak.
Blue Jay Mk.2 – improved version with PbTe IR sensor with hemispherical nose, intended for DH.110, Hunter and Javelin for 1958. Some test firings but became test vehicle for Mk.4.
Blue Jay Mk.2A – proposal of Mk.2 with de-rated motor to reduce max speed.
Blue Jay Mk.3 – as Mk.2 with larger wings for launch at M1.7 at 60,000ft, intended for P.1B and SR53 for 1959. In August 1956 was proposed in two versions; semi-active radar guided (for RN) and IR-guided. Cancelled in 1957 to free development effort for Mk.4.
Blue Jay Mk.4 (Blue Vesta) – PbTe IR-seeker with look angle limited to 60° and larger wings of Mk.3 for launch at M2.0 at 60,000ft for 1961. In September 1956 was proposed in two versions; X-band CW homing with original Mk.1 wings for Sea Vixen and IR-guided with larger wings for 15,000-65,000ft altitude clearance for P.1B and P.177.
Blue Jay Mk.5 (Blue Dolphin) – re-designation of low-altitude CW-homer Mk.4 in July 1957, cancelled later that year.
Red Top – further development of Mk.4 from 1958 with an InSb IR sensor, entered service.
Red Top Mk.2 – May 1960 proposal to replace the solid fuel Linnet motor with a liquid fuel to improve shelf life and handling and improve thrust, proposed as a retrofit for existing missiles.
Red Top Mk.2 Plus – Mk.2 with an enlarged mid-section with a larger boost motor to improve speed to engage high-speed targets.
Radar Red Top – further development of Mk.5 during 1960-61 with a GEC CW seeker, effective at altitudes below 45,000ft and intended mostly for Sea Vixen.
Radar Red Top – 1964 proposal to fit the Matra 530 guidance head
Blue Jay Mk.2A - What did a de-rated motor and reduced max speed bring the the party?
this is great stuff! housings, avionics data, performance data, how did you get all this?All from Lightning F.53 Pilots Notes & DEFE 69/489.
First, performance in Lightning F.53 Pilots Notes:
Maximum overload: 12G lateral acceleration / 7.5G without wings (20G when engine burning according to another source but not authoritative: http://www.loneflyer.com/2020/05/08/hawker-siddeley-red-top/) and rate of roll 30°/sec
Motor Burn time: 2.5 sec (basically 3 sec, you can search the thread about Linnet rocket engine in this forum - there is a document about it)
Max flight time: 30 sec
Seeker FOV: 5° / After launch warning: 1°
Seeker gimbal limit pre-launch: 30° unslaved; 30° slaved by AI23S (export version of AI23B), seeker "looking axis" parallel to A1 scanner axis
Seeker gimbal limit (post-launch): should be above 30°
Warhead explosive mass: 40lbs/18.14kg ( and there's also continous rod)
Proximity fuse range: 40ft/12m
( Here also mentioned "an all-round attack capability")
Nice!Lightning F.53 Pilots Notes:
DEFE 69/489:
Given that I wrote a book on the P.1121 you can draw your own conclusionsNice!Lightning F.53 Pilots Notes:
DEFE 69/489:
Would you by any chance have any manuals to do with the Saro SR.177 and/or the Hawker P.1121?
I don't have a copy of your book and I'd love purchase a copy so please get your publisher to print another run.Given that I wrote a book on the P.1121 you can draw your own conclusions
Will you post that on this forum?I have quite a lot of AI23 stuff that didn't make the p.1121 book.
Interesting. Sounds like Group Captain Burges had a brainstorming session in April 1962.Here the mention of R530 seeker from April 1962.
Any progress about the "20g" problem?The real problem is that, after many years, some web-sources disappeared... I will search for it in my archive, I'm also always interested in real data.
No. Why bother, when Rapier was just around the corner?Does anyone know if there was ever any investigation into a ground launched Red Top akin to the MIM-72 Chaparral?
No. Why bother, when Rapier was just around the corner?Does anyone know if there was ever any investigation into a ground launched Red Top akin to the MIM-72 Chaparral?
The British were primarily worried about big bombers so they concentrated on heavy SAMs the same as the US did. They next worried about aircraft attacking their field armies so they developed a radar guided medium SAM (Thunderbird) and they then worried about low level attack and so Rapier was developed.No. Why bother, when Rapier was just around the corner?Does anyone know if there was ever any investigation into a ground launched Red Top akin to the MIM-72 Chaparral?
It could've been developed quickly as an interim short-range SAM.
Not much point.I suppose a tandem launch booster could've been developed for a surface launched version.
but its pretty useless against a MiG-21 at 500ft from any direction.
but its pretty useless against a MiG-21 at 500ft from any direction.
500Ft? Are you talking about just firing at a MiG-21 from 500Ft (Well within the minimum firing firing distance of a Red Top) or 500Ft altitude?
Where would it be illuminated from though?Red Top with GAR-3 seeker probably was more appropriate for Lightning.
Red Top with GAR-3 seeker probably was more appropriate for Lightning.
For one, the GAR-3 was crude for a SARH, and like any fighter that would have a radar, integration of an illuminator is just one of the hurdles to such a change. Its not like Lightning wasn't around long enough to have figured it out.What makes you think the AIM-4E's seeker mounted on the Red Top would be better? Did the Lightning's AI radar have the room for an illuminator for a SARH missile?
One of the early replies to this thread is a scan of DEFE 69/489 which is basically the MOD evaluating whether to use Red Top or AIM-9D on the Phantom (do note however that they do not have fully detailed information available on either missile at the time of the discussion). The basic conclusion is that there Red Top has front aspect capability (which AIM-9D lacks) and a more lethal warhead, but AIM-9D is probably a bit better in the rear aspect. Ultimately the much increased weight and cost of Red Top swings them in favour of the AIM-9D.I know they serve somewhat different purposes, but how did Red Top compare to pre-L Sidewinders?
The Red Top does indeed have worse kinematic performance than the AIM-9D (particularly at low altitude). The seeker however is much more capable (limited all-aspect capability, better gimbal limits, ability to be slaved off-boresight prior to launch), and the Warhead is larger / more lethal.I have trouble comparing some of the diagrams in this threat with these of AIM-9s, but it almost seems like Red Top has a lower kinematic range than AIM-9D? And that is not even getting into the sensor stuff and endgame performance.
I think the IR Red Top was adequate for the Lightning's needs, it provided all-aspect capability against supersonic bombers and a SARH seeker would have been susceptible to ECM.Red Top with GAR-3 seeker probably was more appropriate for Lightning.
AIM-4E and, for that matter, AIM-9C didn't use a separate illuminator, and got their illumination from the launcher's pulse radar.What makes you think the AIM-4E's seeker mounted on the Red Top would be better? Did the Lightning's AI radar have the room for an illuminator for a SARH missile?
With 4 CW-illuminated Sparrows (Which have a Home on Jam mode) for head-on shots, I doubt that there would be anything to gain from substituting Red Tops for the AIM-9sI'm just trying to imagine the F-4K and F-4M armed with Red Tops instead of AIM-9s.