Maule M-5: Difference between revisions
m Robot - Moving category United States sport aircraft 1970–1979 to Category:1970s United States sport aircraft per CFD at Wikipedia:Categories for discussion/Log/2019 April 19. |
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==Specifications (M-5-235C Strata Rocket)== |
==Specifications (M-5-235C Strata Rocket)== |
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{{Aircraft specs |
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{{aerospecs |
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|ref=The Illustrated Encyclopedia of Aircraft<ref>Orbis 1985, p 2435</ref> |
|ref=The Illustrated Encyclopedia of Aircraft<ref>Orbis 1985, p 2435</ref> |
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|prime units? = imp |
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|met or eng?=<!-- eng for US/UK aircraft, met for all others -->eng |
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|crew=1 |
|crew=1 |
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|capacity=3 |
|capacity=3 |
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|span ft=30 |
|span ft=30 |
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|span in=10 |
|span in=10 |
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|swept m=<!-- swing-wings --> |
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|swept ft=<!-- swing-wings --> |
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|swept in=<!-- swing-wings --> |
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|rot number=<!-- helicopters --> |
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|rot dia m=<!-- helicopters --> |
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|rot dia ft=<!-- helicopters --> |
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|rot dia in=<!-- helicopters --> |
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|dia m=<!-- airships etc --> |
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|dia ft=<!-- airships etc --> |
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|dia in=<!-- airships etc --> |
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|width m=<!-- if applicable --> |
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|width ft=<!-- if applicable --> |
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|width in=<!-- if applicable --> |
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|height m=1.89 |
|height m=1.89 |
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|height ft=6 |
|height ft=6 |
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|height in=2 |
|height in=2.5 |
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|wing area sqm=14.67 |
|wing area sqm=14.67 |
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|wing area sqft=157.90 |
|wing area sqft=157.90 |
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|swept area sqm=<!-- swing-wings --> |
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|swept area sqft=<!-- swing-wings --> |
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|rot area sqm=<!-- helicopters --> |
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|rot area sqft=<!-- helicopters --> |
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|volume m3=<!-- lighter-than-air --> |
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|volume ft3=<!-- lighter-than-air --> |
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|aspect ratio=<!-- sailplanes --> |
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|empty weight kg=635 |
|empty weight kg=635 |
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|empty weight lb=1400 |
|empty weight lb=1400 |
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|gross weight kg=1043 |
|gross weight kg=1043 |
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|gross weight lb=2300 |
|gross weight lb=2300 |
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|lift kg=<!-- lighter-than-air --> |
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|lift lb=<!-- lighter-than-air --> |
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|eng1 number=1 |
|eng1 number=1 |
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|eng1 |
|eng1 name=[[Lycoming O-540|Lycoming O-540-J1A5D]] flat-six piston engine |
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|eng1 kw=<!-- prop engines -->175 |
|eng1 kw=<!-- prop engines -->175 |
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|eng1 hp=<!-- prop engines -->235 |
|eng1 hp=<!-- prop engines -->235 |
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|eng1 kn=<!-- jet/rocket engines --> |
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|eng1 lbf=<!-- jet/rocket engines --> |
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|eng1 kn-ab=<!-- afterburners --> |
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|eng1 lbf-ab=<!-- afterburners --> |
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|eng2 number= |
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|eng2 type= |
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|eng2 kw=<!-- prop engines --> |
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|eng2 hp=<!-- prop engines --> |
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|eng2 kn=<!-- jet/rocket engines --> |
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|eng2 lbf=<!-- jet/rocket engines --> |
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|eng2 kn-ab=<!-- afterburners --> |
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|eng2 lbf-ab=<!-- afterburners --> |
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|max speed kmh=277 |
|max speed kmh=277 |
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|max speed mph=172 |
|max speed mph=172 |
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|max speed mach=<!-- supersonic aircraft --> |
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|cruise speed kmh=<!-- if max speed unknown --> |
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|cruise speed mph=<!-- if max speed unknown --> |
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|range km=885 |
|range km=885 |
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|range miles=550 |
|range miles=550 |
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|endurance h=<!-- if range unknown --> |
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|endurance min=<!-- if range unknown --> |
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|ceiling m=6096 |
|ceiling m=6096 |
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|ceiling ft=20000 |
|ceiling ft=20000 |
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|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
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|climb rate ftmin= |
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|sink rate ms=<!-- sailplanes --> |
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|sink rate ftmin=<!-- sailplanes --> |
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|armament1= |
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|armament2= |
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|armament3= |
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|armament4= |
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|armament5= |
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|armament6= |
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}} |
}} |
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Revision as of 21:28, 23 July 2020
M-5 | |
---|---|
Maule M-5-235C | |
Role | Four-seat cabin monoplane |
National origin | United States |
Manufacturer | Maule Aircraft Company |
Designer | Belford Maule |
First flight | 1971 |
Introduction | 1974 |
Produced | 1974-1983 |
Number built | over 855 |
Developed from | Maule M-4 |
The Maule M-5 is an American four-seat cabin monoplane designed and built by the Maule Aircraft Company.
Design and development
The M-5 was a development of the earlier Maule M-4 with improved STOL performance. It has a 30% increase in flap area and enlarged tail surfaces.
Two prototype M-5s flew in 1971, one powered by a 210-hp (157 kW) engine, the other with a 220-hp (164 kW) engine.
The M-5 is a steel-tube and fabric high-wing braced-monoplane with a cantilever tailplane with a single fin and rudder. It has a fixed-tailwheel landing gear and an enclosed cabin with two rows of side-by-side seating for a pilot and three passengers. The aircraft entered production in 1974 and was named the Strata Rocket and the Lunar Rocket. A generally similar M-6 Super Rocket was also developed with a 3-foot-longer (0.91 m) wingspan and more fuel capacity, smaller ailerons and larger flaps.
Variants
- M-5-180C
- Initial production variant with a 180-horsepower (134 kW) Lycoming O-360-C1F engine, more than 94 built.
- M-5-200
- One aircraft modified with a 200-horsepower (149 kW) engine.
- M-5-210C Strata Rocket
- 180C with a 210-horsepower (157 kW) Continental IO-360-D engine in a revised cowling, 206 built.
- M-5-210TC Lunar Rocker
- 210C fitted with a turbocharged 210-horsepower (157 kW) Lycoming TO-360 engine, 10 built.
- M-5-220C Lunar Rocket
- 210C fitted with a 220-horsepower (164 kW) Franklin 6A-350-C1 engine, 57 built.
- M-5-235C Lunar Rocket
- 210C fitted with a 235-horsepower (175 kW) Lycoming O-540-J1A5D engine, more than 379 built.
- M-6-235C Super Rocket
- 235C with a 3-foot-longer (0.91 m) wingspan and more fuel capacity, smaller ailerons and larger flaps, 136 built.
Specifications (M-5-235C Strata Rocket)
Data from The Illustrated Encyclopedia of Aircraft[1]
General characteristics
- Crew: 1
- Capacity: 3
- Length: 23 ft 6 in (7.16 m)
- Wingspan: 30 ft 10 in (9.40 m)
- Height: 6 ft 2.5 in (1.89 m)
- Wing area: 157.90 sq ft (14.67 m2)
- Empty weight: 1,400 lb (635 kg)
- Gross weight: 2,300 lb (1,043 kg)
- Powerplant: 1 × Lycoming O-540-J1A5D flat-six piston engine , 235 hp (175 kW)
Performance
- Maximum speed: 172 mph (277 km/h, 149 kn)
- Range: 550 mi (885 km, 480 nmi)
- Service ceiling: 20,000 ft (6,096 m)
References
- ^ Orbis 1985, p 2435
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
- Simpson, R.W. Airlife's General Aviation. England: Airlife Publishing. p. 190. ISBN 1-85310-194-X.
{{cite book}}
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(help) - The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. 1985.
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(help)