M-21 Dromader Mini
Role Agricultural aircraft
National origin Poland
Manufacturer WSK-Mielec
Designer Jarosław Rumszewicz[1]
First flight June 18, 1982[2][3]
Number built 2
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

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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

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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

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Data from PZL M-21 Dromader Mini, p. 17

General characteristics

Performance

See also

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Related development

Notes

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References

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  1. ^ a b c d e f PZL M-21 Dromader Mini, p. 17
  2. ^ a b c Taylor 1993, p.963
  3. ^ a b Simpson 1995, p.316
  4. ^ PZL M21 Lama, p.1
  5. ^ Lambert, Munson & Taylor 1991, p. 193
  6. ^ a b c Witkowski 1983, p.5
  7. ^ Glass 1983, p.6–7
  8. ^ a b c Luto
  9. ^ a b c d e Taylor 1984, p.178
  10. ^ PZL M21 Lama, p.16
  11. ^ Glass 2009, p.8
  12. ^ a b PZL M-21 Dromader Mini, p. 18

Bibliography

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