Accrisius FN-10 (cancelled in favour of SP-20 design)
Aircraft Type or Name:
Accrisius FN-10 Tornado
General Type:
Airplane = 1
Airship = 2
Orbiter = 3
1
Year of First Flight: 1933
Description
Carrier or Rough Field
Monoplane
Conventional Fuselage
A monoplane carrier-based fighter aircraft. Armament four wing mounted 7.7mm Mg and two fuselage mounted 13mm HMG and two 500lb bombds underwing.
Characteristics:
Weight (maximum) 10,200 lbs
Weight (empty) 7,660 lbs
Length 38.5 ft
Wingspan 47 ft
Wing Area 323 sq ft
Sweep 8 degrees
Engines 1
Spartan 1000
Piston
1,000 hp
at 5,000 ft
Crew 1
Typical cost $0.031 million in 1934
Total number procured 500
Performance:
Top Speed 194 kts = 223 mph
at 15,000 ft
Mach N/A
Operational Ceiling 22,300 ft
Range 699 nm = 805 miles
with 1,140 lbs payload
1,211 lbs released at halfway point
Climb 1,021 fpm
Cruise 174 kts = 200 mph
at 15,000 ft
Corner Speed 223 KIAS =
224 kts at 500 ft
Mach N/A
Turning Rate 30.0 deg/sec
Radius 1,444 ft
Internal Data:
Intake / Fan Diameter 8 ft
Bypass Ratio 79
Engine Weight 1045 lbs
Overall Efficiency 22.5 percent
Structural Factor 0.95
Number of Wings 1
Number of Fuselages 1
Limiting Airspeed 300 kts
Wing Ultimate g Load 9.00 g
Wing Taper 0.3
Wing Thickness at Root 1.2 ft
Tail / Canard Factor 0.4
Number of Nacelles 0
Length 0 ft
Diameter 0 ft
Fullness 0
Fuselage Diameter 5 ft
Fuselage Fullness 0.4
Pressurized Volume 0 percent
Cargo Decks 1
Cleanness 57 percent
Unstreamlined section 2.4 sq ft
User equipment 2,030 lbs