Engineering:Bradley BA-300 Himat
| BA-300 Himat | |
|---|---|
| Role | Homebuilt aircraft |
| National origin | United States |
| Manufacturer | Bradley Aerospace |
| Introduction | mid-1990s |
| Status | Not built |
The Bradley BA-300 Himat was a proposed United States canard homebuilt aircraft from Bradley 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 the prototype stage.[1]
Design and development
The BA-300 Himat was to have featured a canard layout, with three seats in an enclosed cabin and pusher 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]
Operational history
In April 2015 no examples were registered in the United States with the Federal Aviation Administration.[2]
Specifications (BA-300 Himat)
Data from AeroCrafter[1]
General characteristics
- Crew: one
- Capacity: two passengers
- Fuel capacity: 100 U.S. gallons (380 L; 83 imp gal)
- Powerplant: 1 × aircraft engine
Performance
- Cruise speed: 400 mph (640 km/h, 350 kn)
- Stall speed: 60 mph (97 km/h, 52 kn)
- Range: 3,000 mi (4,800 km, 2,600 nmi)
References
- ↑ 1.0 1.1 1.2 1.3 Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 347. BAI Communications, 15 July 1998. ISBN:0-9636409-4-1
- ↑ Federal Aviation Administration (18 April 2015). "Make / Model Inquiry Results". http://registry.faa.gov/aircraftinquiry/AcftRef_Results.aspx?Mfrtxt=&Modeltxt=BA-300&PageNo=1. Retrieved 18 April 2015.
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