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Continental KB-1

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Continental KB-1

Development and Origins

In 1916, Continental Aircraft Corp. from New York built the Continental KB-1 reconnaissance aircraft for the US Army Signal Corp. The project’s development was led by the young Vincent Justus Burnelli. This aircraft was an early attempt at meeting military aviation needs.

Technical Specifications

The KB-1 was a two-seater, two-strut biplane, powered by a 135 hp Hall-Scott A-5A engine. It featured a three-blade Paragon pusher propeller, a somewhat innovative design for its time. The aircraft was also equipped with distinctive four-wheel Ackerman landing gear.

Trials and Final Fate

Despite successful trials, the military showed no interest in the machine, and consequently, serial production was never initiated. This lack of adoption marked the end of the KB-1’s potential career.

Technical Specifications

Modification KB-1
Wingspan, m 10.97
Length, m 6.71
Height, m 3.12
Empty weight 680
Maximum takeoff weight 1179
Fuel, l 170
Engine type 1 Piston engine Hall-Scott A-5A
Power, hp 1 x 135
Maximum speed, km/h 153
Cruising speed, km/h 116
Flight endurance, h 4
Crew 2

Image gallery of the Continental KB-1

Continental Aircraft Corp.United States
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