Breda - Kingdom of Italy
Manufacturer(s)
Kingdom of Italy; Imperial Japan
Operators
1930
Service Year
Kingdom of Italy
National Origin
Retired
Project Status
2
Crew
4
Units
X-PLANE
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
RUGGED AIRFRAME
Inherent ability of airframe to take considerable damage.
HIGH-SPEED PERFORMANCE
Can accelerate to higher speeds than average aircraft of its time.
HIGH-ALTITUDE PERFORMANCE
Can reach and operate at higher altitudes than average aircraft of its time.
EXTENDED RANGE PERFORMANCE
Capability to travel considerable distances through onboard fuel stores.
SUPER PERFORMANCE
Design covers the three all-important performance categories of speed, altitude, and range.
BAILOUT PROCESS
Manual process of allowing its pilot and / or crew to exit in the event of an airborne emergency.
22.2 ft
(6.78 meters)
Length
30.8 ft
(9.40 meters)
Width/Span
948 lb
(430 kilograms)
Empty Weight
1,830 lb
(830 kilograms)
Maximum Take-Off Weight
+882 lb
(+400 kg)
Weight Difference
monoplane / low-mounted / straight
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Low-Mounted
Mainplanes are low-mounted along the sides of the fuselage.
Straight
The planform involves use of basic, straight mainplane members.
1 x de Havilland Gipsy III 4-cylinder inline, air-cooled piston engine developing 120 horsepower driving two-bladed propeller unit at the nose.
Propulsion
143 mph
(230 kph | 124 knots)
Max Speed
22,966 ft
(7,000 m | 4 miles)
Ceiling
1,118 miles
(1,800 km | 972 nm)
Range
874 ft/min
(266 m/min)
Rate-of-Climb
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030