PZL M-21 Dromader Mini

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M-21 Dromader Mini
PZL-Mielec M-21 Dromader Mini SP-YFK OTT 2013 06.jpg
Role Agricultural aircraft
National origin Poland
Manufacturer WSK-Mielec
DesignerJarosław Rumszewicz [1]
First flightJune 18, 1982 [2] [3]
Number built2
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]

Contents

Development

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

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

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

General characteristics

Performance

See also

Related development

Notes

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References

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

Bibliography