Difference between revisions of "Banyan BA-1"
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|program cost = <!--Total program cost--> | |program cost = <!--Total program cost--> | ||
|unit cost = <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> | |unit cost = <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> | ||
| − | |developed from =[[ | + | |developed from =[[Ki-15 |
|variants with their own articles = <!--Variants OF this aircraft--> | |variants with their own articles = <!--Variants OF this aircraft--> | ||
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Revision as of 17:04, 29 August 2023
{{Infobox aircraft type
| BA-1 | |||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| type = Target drone | national origin = Baltanla | manufacturer = Banyan Aircraft Corporation | designer = | first flight = | introduced = | retired = | status = | primary user = Baltanian Air Force | more users = | produced = | number built = | program cost = | unit cost = | developed from =[[Ki-15 | variants with their own articles =
}} |
The Banyan BA-1 was a target drone developed in the [[Federal States of Baltanla|Baltanla], from Ki-15 fighters withdrawn from manned use at the end of their service life.
Guidance and control equipment was installed in the cockpit in lieu of the ejection seat, with the BA-1 being used for the training of fighter pilots and surface-to-air missile crews.
Operators
Specifications (BA-1
General characteristics
- Crew: 0
- Length: 10.11 m (33 ft 2 in)
- Wingspan: 10.08 m (33 ft 1 in)
- Height: 3.7 m (12 ft 2 in)
- Wing area: 20.6 m2 (222 sq ft)
- Airfoil: TsAGI S-10 / TsAGI SR-3
- Empty weight: 3,630 kg (8,003 lb)
- Gross weight: 5,015 kg (11,056 lb)
- Max takeoff weight: 6,105 kg (13,459 lb)
- Fuel capacity: 1,420 L (312.4 imp gal; 375.1 US gal)
- Powerplant: 1 × Klimov VK-1 centrifugal flow turbojet, 26.5 kN (6,000 lbf) thrust
Performance
- Maximum speed: 1,076 km/h (669 mph, 581 kn) at sea level
- 1,033 km/h (558 kn; 642 mph) at 5,000 m (16,000 ft)
- 992 km/h (536 kn; 616 mph) at 10,000 m (33,000 ft)
- Maximum speed: Mach 0.87
- Cruise speed: 850 km/h (530 mph, 460 kn)
- Range: 1,240 km (770 mi, 670 nmi)
- Service ceiling: 15,500 m (50,900 ft)
- Rate of climb: 51.2 m/s (10,080 ft/min) at sea level
- 36.2 m/s (7,130 ft/min) at 5,000 m (16,000 ft)
- 21 m/s (4,100 ft/min) at 10,000 m (33,000 ft)
- Time to altitude: 5,000 m (16,000 ft) in 2 minutes
- 10,000 m (33,000 ft) in 5.2 minutes
- Wing loading: 240.8 kg/m2 (49.3 lb/sq ft)
- Thrust/weight: 0.00534 kN/kg (0.544 lbf/lb)
Avionics
Remote control / Radio command guidance equipment
