Honda MH02: Difference between revisions
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==See also== |
==See also== |
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* [[VFW-Fokker 614]]: twin overwing jet engines |
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{{aircontent| |
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|sequence= |
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|related= |
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* [[Honda HA-420 HondaJet]] |
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|similar aircraft= |
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|lists= |
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* [[List of civil aircraft]] |
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* [[List of experimental aircraft]] |
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|see also= |
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==Notes== |
==Notes== |
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Revision as of 09:30, 22 June 2020
| MH02 | |
|---|---|
| |
| Role | Experimental aircraft |
| Manufacturer | Honda Mississippi State University |
| First flight | 5 March 1993 |
| Status | Retired |
| Number built | 1 |
| Developed into | Honda HA-420 HondaJet |
The Honda MH02 was an experimental business jet built by Honda, in cooperation with Mississippi State University, to research engine placement and composite construction. The prototype was completed in 1992, making its first flight on 5 March 1993.
The MH02 was never intended for production, but was nonetheless the first all-composite light business jet to fly; by 1996 over 170 test flight hours were accumulated on the airframe. Aside from the already unusual above-the-wing engine mounts, the design features a T-tail and a forward-swept wing.[1] The aircraft was deregistered and exported to Japan in 1998.[2][3]
Specifications (MH02)
General characteristics
- Crew: one or two pilots
- Capacity: six passengers
- Length: 11.25 m (36 ft 11 in)
- Wingspan: 11.24 m (36 ft 11 in)
- Height: 4.18 m (13 ft 9 in)
- Max takeoff weight: 3,600 kg (7,937 lb)
- Powerplant: 2 × Pratt & Whitney Canada JT15D1 turbofan engines, 5.3 kN (1,200 lbf) thrust each
Performance
- Maximum speed: 654 km/h (406 mph, 353 kn)
See also
- VFW-Fokker 614: twin overwing jet engines
Notes
External links
Wikimedia Commons has media related to Honda MH02.
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