Hamburger Flugzeugbau V/STOL Aircraft
Hamburger Flugzeugbau GmbH (Germany)
Hamburger Flugzeugbau GmbH -> MBB (1969)
Y2A Ranger
V/STOL reconnaissance and strike fighter
- Power: Two GE.1 turbojets which provide propulsion and behave as gas generators for the eight lift fans
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HFB 351
V/STOL transport
- Power: Six GE.1 turbojets which provide propulsion and behave as gas generators for the eight lift fans
- Capacity: 80 passengers
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| HFB 530 Ranger |
Lift + Lift/Cruise |
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Lift fan-powered fighter, developed with Ryan. My be identical with Y2A Ranger, see above.
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| HFB 570 |
Lift + Lift/Cruise |
Developed begins 1967 as a V/STOL battle zone transport.
- Lift Power: three gas generators powering four lift fans that deployed from the sides of the fuselage.
- Lift/Cruise Power: four gas generators powering four lift/cruise fans
- Maximum Speed: 916 km/h at 0 m altitude
- Range: 741 km (400 nm)
- Wing span: 21 m (68.9 ft)
- Length: 27 m (88.6 ft)
- Height: 9.15 m (30 ft)
- Empty Weight: 22,250 kg
- Payload: 60 passengers or 8,000 kg
- Maximum VTO Weight: 38,500 kg (84,880 lb)
- 3-side-view with propulsion system
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| HFB 590 "Vertibus" |
Lift + Lift/Cruise |
Developed begins in 1968.
- Lift Power: two lift large fans powered by four gas generators in the fuselage bottom
- Lift/Cruise Power: two fans with gas generators on the wing
- Controll Power: a fan in the tail and at each of the wingtips
- Wing span: 20 m
- Length: 28.5 m
- Height: 7.6 m
- Capacity: 90 passengers
- 3-side-view
- 3-side-view with propulsion system
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| HFB 600 "Vertibus" |
Lift + Lift/Cruise |
Submitted in a proposal to the West German Federal Defence Ministry for an 80-100 passenger V/STOL transport projected for service in late 1970s.
Design circa 1970. Developing a Civilian (Z) and a Military (M) version.
- Lift Power: 4 General Electric GE1/10J1 gas generators powering 4 GE fans under the center of fuselage.
- Lift/Cruise Power: 4 General Electric GE1/10J1 gas generators powering 4 GE fans under the wings.
- Control Power: 4 GE fans: one each at wingtips (Powert by wing engines), tail and nose(Powert by fuselage engines).
- Cruise Speed: 880 km/h (475 kt)
- * Cruise Speed: 990 km/h (535 kt)
- Maximum Speed: 990 km/h (535 kt)
- * Maximum Speed: 1050 km/h
- Maximum Altitude: 10,200 m (33,500 ft)
- Maximum rate of climb: 45 m/s (148 ft/s)
- Range (Z, 91 passengers): 843 km plus reserve
- Range (M, 10,000 kg payload): 900 km plus reserve
- Wing span: 23.8 m (78.1 ft)
- Wing Area: 91.8 meters² (988 ft²)
- Length: 30.8 m (101 ft)
- Height: 10.4 m (34.1 ft)
- Capacity: 77-91 passengers (Z) or 102 troops (M)
- Empty Weight: 33,930 kg (74,800 lb)(Z); 32,360 kg (M)
- Maximum STO Weight: 60,820 kg (M)
- Maximum VTO Weight: 50,520 kg (111,400 lb)
- * Maximum VTO Weight: 55,800 kg
- Maximum Take-off weight: 122,750 lb.
- Fuel load: 7,420 kg (16,360 lb)
- * Fuel load: 12,700 kg
- Payload: 9,170 kg (20,215 lb)
- * Payload: 16,000 kg
- 3-side-view
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