The Bellanca 19-25 Skyrocket II was a prototype light airplane built in the United States in the 1970s by the Bellanca Aircraft Engineering company of Scott Depot, West Virginia, which August Thomas Bellanca, son of Giuseppe Bellanca, formed to develop a design conceived in 1957. It was a six-seat, low-wing cantilever monoplane made of composite materials, with retractable tricycle landing gear and a 435 horsepower Continental GTSIO-520-F engine. In 1975, within months of its first flight, the prototype claimed five world airspeed records for piston aircraft in its class, and NASA studied its aerodynamics to investigate natural laminar flow. Its maximum speed was 331 mph. It never achieved certification or entered production, because plans to build it commercially were scrapped after the downturn in the United States civil aviation market in the early 1980s, and the design later returned as the Skyrocket III kit. The prototype survives at the Bellanca Airfield Museum in New Castle, Delaware.
Facts
Top Speed (km/h) Maximum Mass (kg) EngineContinental GTSIO-520-F 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Bellanca Skyrocket II (Wikipedia)
Of Make
Source Bellanca Skyrocket II (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Bellanca Skyrocket II (Wikipedia)Development, builderQuote, Development, builder
Bellanca formed the Bellanca Aircraft Engineering Inc. company in Scott Depot, West Virginia to develop a new design
Originated In
Also in Geography Atlas: where this subject originated.
Source Bellanca Skyrocket II (Wikipedia)LeadQuote, Lead
The Bellanca 19-25 Skyrocket II was a prototype light airplane built in the United States in the 1970s.
Sources
1. Bellanca Skyrocket II (Wikipedia)
Lead
The Bellanca 19-25 Skyrocket II was a prototype light airplane built in the United States in the 1970s.
Specifications, powerplant
Powerplant: 1 × Continental GTSIO-520-F air-cooled flat-six, 435 hp (324 kW)
Specifications, power
Powerplant: 1 × Continental GTSIO-520-F air-cooled flat-six, 435 hp (324 kW)
Specifications, empty mass
Empty weight: 2,300 lb (1,043 kg)
Specifications, maximum mass
Max takeoff weight: 4,100 lb (1,860 kg)
Specifications, top speed
Maximum speed: 331 mph (533 km/h, 288 kn) at 29,000 ft (8,800 m)
Surviving aircraft
The prototype Skyrocket II was displayed at the Delaware Aviation Museum in Georgetown, Delaware
Development, builder
Bellanca formed the Bellanca Aircraft Engineering Inc. company in Scott Depot, West Virginia to develop a new design
Of Make: Bellanca, Lead, make
The Bellanca 19-25 Skyrocket II was a prototype light airplane built in the United States in the 1970s.
Exemplifies: Aviation, Lead, mode
The Bellanca 19-25 Skyrocket II was a prototype light airplane built in the United States in the 1970s.
In Group: Single-Engine Piston Light Aircraft, Lead, vehicle type
The Bellanca 19-25 Skyrocket II was a prototype light airplane built in the United States in the 1970s.
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