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Data from General characteristics Crew: 1 Length: 3 ft (0.91 m) approx. Height: 4 ft 0 in (1.22 m) Empty weight: 401 lb (182 kg) Gross weight: 550 lb (249 kg) Powerplant: 1 × Williams F107 turbofan engine, 570 lbf (2.5 kN) thrust (modified) Performance Maximum speed: 52 kn (60 mph, 96 km/h) Endurance: 30–45 minutes Service ceiling: 10,000 ft (3,000 m) Thrust/weight: 1.11 See also Aircraft ...
Data from Cliche and Virtual Ultralight Museum General characteristics Crew: one Length: 15 ft 0 in (4.57 m) Upper wingspan: 24 ft 0 in (7.32 m) Lower wingspan: 20 ft 4 in (6.20 m) Height: 6 ft 0 in (1.83 m) Wing area: 160 sq ft (15 m 2) Empty weight: 218 lb (99 kg) Gross weight: 415 lb (188 kg) Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal) Powerplant: 1 × Cuyuna 430R, 30 hp (22 kW ...
Data from Wings of Motherland General characteristics Crew: 2 Length: 10.14 m (33 ft 3 in) Wingspan: 9.38 m (30 ft 9 in) Height: 3.4 m (11 ft 2 in) Wing area: 14.3 m 2 (154 sq ft) Airfoil: TsAGI S-9S Empty weight: 1,555 kg (3,428 lb) Gross weight: 2,250 kg (4,960 lb) Max takeoff weight: 2,550 kg (5,622 lb) Fuel capacity: 500 kg (1,100 lb) Powerplant: 1 × Tumansky RU-19-300 turbojet engine, 10 ...
Quickest 0 to 97 km/h (0 to 60 mph) with 1 foot rollout – 1.74 seconds – Rimac Nevera [54] Quickest 0 to 100 km/h (0 to 62 mph) with 1 foot rollout – 1.81 seconds – Rimac Nevera [54] Quickest 0 to 161 km/h (0 to 100 mph) with 1 foot rollout – 3.21 seconds – Rimac Nevera [54]
Data from Jane's All the World's Aircraft 2011/12., Sport Aviation June 2012, manufacturer. General characteristics Capacity: 4 (pilot and three passengers) Length: 7.97 m (26 ft 2 in) Wingspan: 10.30 m (33 ft 10 in) Height: 2.64 m (8 ft 8 in) Wing area: 13.90 m 2 (149.6 sq ft) Airfoil: NACA 63A Empty weight: 818 kg (1,803 lb) Max takeoff weight: 1,220 kg (2,690 lb) Fuel capacity: 240 L (46.2 ...
The car is 16.50 m (54.1 ft) long and 3.7 m (12 ft) wide and has a curb weight of 10.6 tons. It had a reported thrust of 223 kN (approximately 50,000 pounds force) at some operating condition. Jet engines are not designed to operate at peak airspeed while still in ground effect ; a proper estimate would need to take this into account.
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