Transport Atlas

How The World Moves
Sign In
Text size
100%
Theme
Vehicle

Bellanca Skyrocket II

General Aviation and Light Aircraft

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
Status
Surviving 1
Status
Prototype 1
Power (kW)
324 1
Top Speed (km/h)
533 1
Mass (kg)
1043 1
Maximum Mass (kg)
1860 1
Engine
Continental GTSIO-520-F 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
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, builder
Quote, 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)Lead
Quote, 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.
View the Source
Comments (0)
No comments yet. Be the first to share a thought.
Reader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.