Skandinaviska Aero BHT-1 Beauty
The Skandinaviska Aero BHT-1 Beauty is a 1940s Swedish single-seat light monoplane designed by E. Bratt, K.E. Hilfing and B.Törnblom and built by Skandinaviska Aero of Stockholm.
| BHT-1 Beauty | |
|---|---|
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| Role | Single-seat light monoplane | 
| National origin | Sweden | 
| Manufacturer | Skandinaviska Aero | 
| Designer | E. Bratt, K.E. Hilfing and B.Törnblom | 
| First flight | 4 December 1944 | 
| Number built | 1 | 
Design
    
The BHT-1 is a wooden low-wing cantilever monoplane with a retractable tailwheel landing gear. Powered by a 60 hp (45 kW) Walter Mikron 4 piston engine it has an enclosed single-seat cockpit. The wings include slotted flaps.[1]
Variants
    
The BHT-2 was a proposed two-seat development. A prototype constant speed propeller was developed for the aircraft using differential between engine oil, and ram air pressure to control pitch.[1]
Specifications
    
Data from Jane's Fighting Aircraft of World War II,[2] Jane's all the World's Aircraft 1947[3]
General characteristics
- Crew: 1
 - Length: 5.8 m (19 ft 0 in)
 - Wingspan: 6.82 m (22 ft 5 in)
 - Height: 1.9 m (6 ft 3 in)
 - Wing area: 7 m2 (75 sq ft)
 - Empty weight: 240 kg (529 lb)
 - Gross weight: 365 kg (805 lb) aerobatic
 - Max takeoff weight: 420 kg (926 lb) long-range
 - Fuel capacity: 88 l (23 US gal; 19 imp gal) in three tanks, plus 127 l (34 US gal; 28 imp gal) in "special reserve" fuel tank
 - Powerplant: 1 × Walter Mikron 4 4-cyl. inverted air-cooled in-line piston engine, 45 kW (60 hp)
 - Propellers: 2-bladed wooden fixed-pitch airscrew with provision for controllable-pitch airscrew
 
Performance
- Maximum speed: 250 km/h (160 mph, 130 kn)
 - Cruise speed: 210 km/h (130 mph, 110 kn) *Landing speed with flaps:75 km/h (47 mph; 40 kn)
 - Never exceed speed: 580 km/h (360 mph, 310 kn) with controllable-pitch airscrew
 - Range: 1,700 km (1,100 mi, 920 nmi)
 - Ferry range: 3,000 km (1,900 mi, 1,600 nmi) with special reserve fuel tank
 - Service ceiling: 7,500 m (24,600 ft)
 - Rate of climb: 5.2 m/s (1,020 ft/min)
 - Wing loading: 52 kg/m2 (11 lb/sq ft) aerobatic
 - Power/mass: 8.18 kg/kW (13.42 lb/hp)
 
References
    
- "Capt. Jan Christie's BHT-1". Experimenter. June 1955.
 - Bridgman, Leonard (1988). Jane's Fighting Aircraft of World War II. New York: Crescent Books. p. 288. ISBN 0-517-67964-7.
 - Bridgman, Leonard, ed. (1947). Jane's all the World's Aircraft 1947. London: Sampson Low, Marston & Co. p. 166c.
 
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