| Variant |
Engines/Thrust |
Weights |
Dimensions |
Distinguishing Features |
| P.1A |
2 x Armstrong-Siddeley Sapphire Sa5, 7,500lb each: later replaced
by Sapphire 5R 9,200lb with reheat |
22,221lb Empty
27,077lb Loaded |
Span: 34ft 10in
Lenght: 49ft 8in;
Height: 17ft 3in;
Wing area: 458.5sqft |
Original prototypes to F23/49 Max speed Mach 1.53 (1,011 mph)
at 36,000 ft |
| P1.B |
2 x Rolls-Royce Avon 200R (later 210R) 14,430lb Each with reheat
|
24,816lb Empty;
31,831lb Loaded;
34,140lb Max loaded; |
Span: 34ft 10in;
Lenght: 55ft 3in;
Height: 19ft 5in;
Wing area: 458.5sqft |
Fighter Prototype,
Max speed Mach 2.1 1,390mph) at 40,000ft |
| Lightning
F.1 |
2 x Rolls-Royce Avon 200R |
25,753lb
Empty |
As P1.B Except
Height: 19ft 7in |
First production version AI 23 radar,VHF radio (Later replaced
by UHF) 2 x 30mm Aden cannon in nose 2 x Firestreak missiles or
alternative weapons pack Mach 2.2 approx |
| Lightning
F.1A |
2 x Rolls-Royce Avon 210R with revised, four position reheat
throttle control |
25,737lb Empty |
As F.1 |
First version with in-flight refueling UHF radio, external
cable ducts to missile pylons |
| Lightning F.2 |
2 x Rolls-Royce Avon 210R with fully variable
reheat control |
27,000lb
Empty |
As F.1 |
Revised cockpit including partial OR946 specification, liquid
oxygen breathing system, standby turbo generator for DC electrical
supply identified by small scoop on dorsal spine |
| Lightning
F.2A |
2 x Rolls-Royce Avon 211R |
27,000lb
Empty |
As F.1 except wing area:
474.5sqft |
F.2 rebuilt to incorporate some F.6 features: kinked, cambered
wing square cut fin, enlarged ventral fuel tank 2 x Aden
cannon (in upper nose) 2 x Firestreak missiles |
| Lightning F.3 |
2 x Rolls-Royce Avon 301R, 12,690lb thrust (dry) and 16,360lb
thrust (reheat) |
26,905lb
Empty |
as F.1 |
Square cut fin of 15% greater area deletion of in-built cannon
more advanced radar AI 23B which allowed either Red Top collision
course missiles or Firestreak. Full OR946 integrated flight system
|
| Lightning
F.3A
(Interim F.6) |
2 x Rolls-Royce Avon 301R, 12,690lb thrust (dry) and 16,360lb
thrust (reheat) |
28,041lb
Empty
41,700lb Loaded |
As F.3 Except wing
474.5sqft |
Kinked, cambered wing for greater area and enlarged ventral
tank |
| Lightning T.4 |
2 x Rolls-Royce Avon 210R |
27,000LB
Empty |
As F.1 |
Two seat, dual control trainer version of F.1A; deletion of
cannon from upper nose |
| Lightning T.5 |
2 x Rolls-Royce Avon 301R |
27,000LB
Empty |
As F.3 |
Two seat, dual control trainer version of F.3 with capability
of carrying either Red Top or Firestreak missiles |
| Lightning F.6 |
2 x Rolls-Royce Avon 301R |
28,041LB Empty
41,700LB max loaded |
As F.3A |
Full production version of F.3A with provision to carry over-wing
fuel tanks and some small improvement to equipment |
| Lightning F.53 |
2 x Rolls-Royce Avon 302C |
Similar to F.6 |
As F.3A |
Export version of F.6 with the capability to carry a wider
range of ordanance from over or under wing pylons AI 23S radar (export
version of AI 23B) |
| Lightning T.55 |
2 x Rolls-Royce Avon 302C |
Similar to F.6 |
As F.3A |
Export version of T.5 with the enlarged ventral tank, kinked
cambered wing and AI 23S |
In the course of its long RAF service, most versions
of Lightning were subject to the incorporation of many modifications,
mostly without significant external evidence of change. Many were concerned
with improving the fire prevention integrity of the engine bays and jet
pipes, where the high incidence of fires caused the loss of a high proportion
of the Lightnings which were written off in flying accidents.
Modifications to operational equipment were relatively
few, because they were not considered cost-effective in an aircraft which
was not expected to remain in service for more than a decade! However,
limited improvements were made to the AI 23B radar, resulting in the AI
23C and finallyAI 23D versions.