PZL M-21 Dromader Mini
| M-21 Dromader Mini | |
|---|---|
| File:PZL-Mielec M-21 Dromader Mini SP-YFK OTT 2013 06.jpg | |
| General information | |
| Type | Agricultural aircraft |
| National origin | Poland |
| Manufacturer | WSK-Mielec |
| Designer | Jarosław Rumszewicz[1] |
| Number built | 2 |
| History | |
| First flight | June 18, 1982[2][3] |
| Developed from | PZL-Mielec M-18 Dromader[2] |
The PZL M-24 Dromader Mini (Dromader is Polish for "Dromedary"), originally named the Lama[4] (Polish for "Llama"), is a single engine agricultural aircraft, developed in the 1980s by WSK-Mielec (later PZL-Mielec) from the PZL-Mielec M-18 Dromader.[2] The prototype, registration SP-PDM, first flew on 18 June 1982.[3] It did not progress beyond the prototyping stage.[5]
Development
[edit | edit source]By the early 1980s, WSK-Mielec was aware that the economics of aerial application in agriculture varied according to the characteristics of the land being treated.[6] One relevant factor was the size of the plot, where a larger aircraft is more cost-effective for treating a larger area of land, and a smaller aircraft more cost-effective for a smaller area.[6] The company therefore decided to manufacture a range of agricultural aircraft of different sizes, based on the already-proven M-18 design.[6][7] This member of the family was intended for smaller areas of land, up to about 50 hectares (120 acres).[8]
The M-21 was designed to retain as much commonality with the M-18 as possible; ultimately around 70% was achieved.[1][9] Common areas included the cabin, rear fuselage, empennage, outer wing panels, and mainwheels.[1][9] The desire to maximise this commonality resulted in an overall weight greater than what would otherwise have been necessary.[10]
Design work commenced in January 1980 and was concluded by June that year.[1] Construction of the first prototype began in August 1981, and it first flew on 18 June 1982.[1] Three prototypes were built: two for flight testing and one for static tests.[1][9]
The prototypes were tested from 1982 to 1986, when the design was certified.[8] However, PZL did not have capacity to manufacture the design alongside the company's existing programs and no further examples were built.[8]
A turboprop version, the M-21T, powered by a Walter M601A, was designed but never constructed.[11]
Design
[edit | edit source]The M-21 is a conventional, low-wing cantilever monoplane with fixed, tailwheel undercarriage.[12] Construction is of metal throughout.[9] It is equipped with a single seat in an enclosed cabin.[9] Power is supplied by a single PZL-3SR radial engine mounted tractor-fashion in the nose.[12]
Specifications
[edit | edit source]Data from PZL M-21 Dromader Mini, p. 17
General characteristics
- Crew: 1 pilot
- Capacity: 1,700 L (450 US gal; 370 imp gal) / 965 kg (2,127 lb) of chemicals
- Length: 9.48 m (31 ft 1 in)
- Wingspan: 14.51 m (47 ft 7 in)
- Height: 3.11 m (10 ft 2 in)
- Wing area: 32.6 m2 (351 sq ft)
- Empty weight: 2,060 kg (4,542 lb)
- Max takeoff weight: 3,300 kg (7,275 lb)
- Powerplant: 1 × PZL-3SR 7-cylinder air-cooled radial piston engine, 442 kW (593 hp)
Performance
- Maximum speed: 187 km/h (116 mph, 101 kn)
- Cruise speed: 180 km/h (110 mph, 97 kn)
- Service ceiling: 2,900 m (9,500 ft)
- Rate of climb: 3.8 m/s (750 ft/min)
See also
[edit | edit source]Related development
Notes
[edit | edit source]References
[edit | edit source]- ^ a b c d e f PZL M-21 Dromader Mini, p. 17
- ^ a b c Taylor 1993, p.963
- ^ a b Simpson 1995, p.316
- ^ PZL M21 Lama, p.1
- ^ Lambert, Munson & Taylor 1991, p. 193
- ^ a b c Witkowski 1983, p.5
- ^ Glass 1983, p.6–7
- ^ a b c Luto
- ^ a b c d e Taylor 1984, p.178
- ^ PZL M21 Lama, p.16
- ^ Glass 2009, p.8
- ^ a b PZL M-21 Dromader Mini, p. 18
Bibliography
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