One thing I've been playing with is the desirability of have air cover not tied to a large expensive carrier, or to if there happens to be a functional airstrip- for example to cover the roads where an amphibious force is off loading while the carrier is free to cover the striking force.
So I've come up with two designs. Both are more geared towards dispersing and downing bombers than mixing it up with fighters.
Both are float biplanes with big radial engines, and wingloading is kept under 20 to allow for easier water landings.
I'm leaning towards the second, as both are slower than current fighters, and that has twin 20mm fore and the turreted rear guns.
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Aircraft Type or Name:
Fokker D.XVIII-W
General Type:
Airplane = 1
Airship = 2
Orbiter = 3
1
Year of First Flight: 1934
Description
Flying Boat / Seaplane
Biplane
Conventional Fuselage
A fighter seaplane. 1x 20mm Hispano, 4x 7.92mm MGs, 10mm armor disk. Provisions for 2x 50kg bomb/DCs. Performance is without payload.
Characteristics:
Weight (maximum) 5,580 lbs
Weight (empty) 4,612 lbs
Length 26 ft
Wingspan 37 ft
Wing Area 295 sq ft
Sweep 2 degrees
Engines 1
Bristol Mercury XV
Piston
995 hp
at 15,000 ft
Crew 1
Typical cost $0.025 million in 1935
Total number procured 64
Performance:
Top Speed 270 kts = 311 mph
at 15,000 ft
Mach N/A
Operational Ceiling 42,000 ft
Range 454 nm = 523 miles
with 322 lbs payload
334 lbs released at halfway point
Climb 2,637 fpm
Cruise 135 kts = 155 mph
at 15,000 ft
Corner Speed 177 KIAS =
222 kts at 15,000 ft
Mach N/A
Turning Rate 32.2 deg/sec
Radius 1,339 ft
Internal Data:
Intake / Fan Diameter 9 ft
Bypass Ratio 91.35
Engine Weight 1065 lbs
Overall Efficiency 22 percent
Structural Factor 1.00
Number of Wings 1.9
Number of Fuselages 1
Limiting Airspeed 280 kts
Wing Ultimate g Load 10.00 g
Wing Taper 0.3
Wing Thickness at Root 0.8 ft
Tail / Canard Factor 0.4
Number of Nacelles 0
Length 6 ft
Diameter 3 ft
Fullness 0.5
Fuselage Diameter 4.6 ft
Fuselage Fullness 0.4
Pressurized Volume 0 percent
Cargo Decks 0
Cleanness 63.2 percent
Unstreamlined section 2.6 sq ft
User equipment 940 lbs
====================
====================
Aircraft Type or Name:
Fokker D.XVIII-W
General Type:
Airplane = 1
Airship = 2
Orbiter = 3
1
Year of First Flight: 1935
Description
Flying Boat / Seaplane
Biplane
Conventional Fuselage
Fighter Floatplane. 2x 20mm, 2x 7.92mm fore, 2x7.92mm turret aft. Armor, radio.
Characteristics:
Weight (maximum) 7,165 lbs
Weight (empty) 6,049 lbs
Length 34.1 ft
Wingspan 40 ft
Wing Area 359 sq ft
Sweep 3 degrees
Engines 1
Avia Pegasus XVIII
Piston
1,065 hp
at 15,000 ft
Crew 2
Typical cost $0.026 million in 1935
Total number procured 144
Performance:
Top Speed 258 kts = 297 mph
at 15,000 ft
Mach N/A
Operational Ceiling 37,500 ft
Range 454 nm = 523 miles
with 114 lbs payload
119 lbs released at halfway point
Climb 1,914 fpm
Cruise 140 kts = 161 mph
at 15,000 ft
Corner Speed 182 KIAS =
218 kts at 12,000 ft
Mach N/A
Turning Rate 31.0 deg/sec
Radius 1,360 ft
Internal Data:
Intake / Fan Diameter 9 ft
Bypass Ratio 87.3
Engine Weight 1036 lbs
Overall Efficiency 22 percent
Structural Factor 1.00
Number of Wings 1.9
Number of Fuselages 1
Limiting Airspeed 280 kts
Wing Ultimate g Load 10.00 g
Wing Taper 0.2
Wing Thickness at Root 0.9 ft
Tail / Canard Factor 0.4
Number of Nacelles 0
Length 6 ft
Diameter 3 ft
Fullness 0.5
Fuselage Diameter 4.8 ft
Fuselage Fullness 0.4
Pressurized Volume 0 percent
Cargo Decks 0
Cleanness 66 percent
Unstreamlined section 2.7 sq ft
User equipment 1,700 lbs