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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