Breda - Kingdom of Italy
Kingdom of Italy; Imperial Japan
Kingdom of Italy
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
Inherent ability of airframe to take considerable damage.
Can accelerate to higher speeds than average aircraft of its time.
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.
Design covers the three all-important performance categories of speed, altitude, and range.
Manual process of allowing its pilot and / or crew to exit in the event of an airborne emergency.
Maximum Take-Off Weight
monoplane / low-mounted / straight
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Mainplanes are low-mounted along the sides of the fuselage.
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.
(230 kph | 124 knots)
(7,000 m | 4 miles)
(1,800 km | 972 nm)
MACH Regime (Sonic)
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030