| BA-300 Himat | |
|---|---|
| General information | |
| Type | Homebuilt aircraft |
| National origin | United States |
| Manufacturer | Bradley Aerospace |
| Status | Not built |
| History | |
| Introduction date | mid-1990s |
TheBradley BA-300 Himat was a proposedAmericancanardhomebuilt aircraft fromBradley Aerospace, introduced in the mid-1990s. The aircraft was to have been supplied as a kit for amateur construction, but it does not seem to have progressed to theprototype stage.[1]
The BA-300 Himat was to have featured a canard layout, with three seats in an enclosed cabin andpusher configuration. It was to have a cruise speed of 400 mph (640 km/h).[1]
The BA-300 was to fit a belly tank that would hold 100 U.S. gallons (380 L; 83 imp gal) of fuel to allow a range of over 3,000 mi (4,800 km). The belly tank was to have also been convertible for other uses, including plans for drop-doors.[1]
In April 2015 no examples wereregistered in the United States with theFederal Aviation Administration.[2]
Data from AeroCrafter[1]
General characteristics
Performance