wuzak
Captain
The main difference between the Type 324 and Type 327 is that the former's 12 x 0.303" in the outer wing panels were replaced by 6 x 20mm cannon in the wing roots, as the 327 was proposed to as a cannon armed fighter.
The engine choices were the Merlin RM.2SM (Mk X??) and the Taurus TE-3SM.
The engine performances:
Merlin RM.2SM
Fuel: 100 octane
Supercharger Gear | High | Low |
Maximum Power (bhp) | 1,145 | 1,265 |
at Altitude (ft) | 16,750 | 9,500 |
International Rating (bhp) | 1,135 | 1,250 |
at Altitude (ft) | 15,500 | 8,000 |
Power at Economical Cruising Speed @ 15,000ft (bhp) | - | 233 |
Take-off Power (bhp) | - | 1,300 |
RPM | - | 3,000 |
Reduction Gear | 0.42 | 0.42 |
Dry Weight (lb) | 1,390 | 1,390 |
Taurus TE-3SM
Fuel: 100 octane
Supercharger Gear | High | Low |
Maximum Power (bhp) | 1,165 | 1,250 |
at Altitude (ft) | 15,000 | 5,000 |
International Rating (bhp) | 980 | 1,080 |
at Altitude (ft) | 15,000 | 5,000 |
Power at Economical Cruising Speed @ 15,000ft (bhp) | - | 226 |
Take-off Power (bhp) | - | 1,200 |
RPM | - | 3,300 |
Reduction Gear | 0.444 | 0.444 |
Dry Weight (lb) | 1,345 | 1,345 |
Estimated performance:
Engines | Merlin | Taurus |
All Up Weight (lb) | 11,312 | 10,536 |
Maximum Speed (mph) | 465 | 430 |
at altitide (ft) | 22,000 | 20,000 |
Speed at 15,000ft (mph) | 423 | 404 |
Economical Cruising Speed (mph) | 210 | 195 |
at altitide (ft) | 15,000 | 15,000 |
Service Ceiling | 40,000 | 35,500 |
Take-off Over 50ft, no wind (yd) | 409 | 465 |
Landing Over 50ft, no wind (yd) | 439 | 393 |
The wing had a span of 40ft and wing area of 304sq.ft. It was fitted with Fowler Flaps which covered 57.5% of the span.
The wing was structurally very similar to the Spitfire's. It was described has having a single spar at the maximum thickness. It was built in 5 sections:
The centre section was built with the fuselage and contained the 6 20mm cannon installation.
The mid sections contained the engine, the radiator (buried in the wing outboard of the engine, fed from a leading edge intake), the main landing gear (folding inwards), the Fowler flaps and mechanisms and fuel tanks in the leading edge inboard of the engine (68 UKG each, and forming part of the structure) and in the engine nacelle (42 UKG each).
The outer wing panels contained the ailerons. These could be swapped for panels conaining 6 0.303" mgs for the ground attack role.
The wing section was of the NACA 2200 family, as was the Spitfire's.
The basic dimensions were:
Engines | Merlin | Taurus |
Span (ft) | 40 | 40 |
Gross Area (sq.ft) | 304 | 304 |
Length Overall (ft) | 33.5 | 33.5 |
Height on Wheels (static) (ft) | 9.75 | 9.75 |
Chassis Track (ft) | 12.5 | 12.5 |
Wheelbase (ft) | 9 | 9 |
Airscrew Diameter (ft) | 10.3 | 8.75 |
The weight break down was:
Engines | Merlin | Taurus |
Structure (lb) | 3,776 | 3,696 |
Power Plant (lb) | 4,410 | 3,809 |
Load | 3,126 | 3,031 |
All Up Weight | 11,312 | 10,536 |
The breakdown of the load was:
Engines | Merlin | Taurus |
Pilot and Parachute | 200 | 200 |
Fixed Military Load | 583 | 583 |
Removeable Load | 875 | 875 |
Fuel (at 7.2lb/UKG) | 1,225 | 1,265 |
Oil | 243 | 108 |
Load | 3,126 | 3,031 |
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