Miles Martinet Aircraft

Production Details

Design Company:

Phillips & Powis Aircraft Ltd

First Flight:

24 April 1942

M.25 Martinet:

1,726 - Phillips & Powis, Woodley

M.37 Martinet Trainer:

2 - Miles Aircraft Ltd

M.50 Queen Martinet:

65 - Phillips & Powis, Woodley

Type Specification

Applies to:

Miles M.25 Martinet

Type:

Target tug to specification 12/41 based on Master trainer

Wing:

Low wing cantilever monoplane of spruce structure covered in plywood. Split flaps fitted as standard

Fuselage:

Fuselage of spruce structure with plywood covering

Tail Unit:

Cantilever tailplane with elevator at top of fuselage with single fin and rudder

Landing Gear:

Single wheel on each main leg, which retract into wing. Tailwheel

Power Plant:

One 870 hp Bristol Mercury XX radial engine in the nose

Accommodation:

Tandem seats for crew in enclosed cockpit

Span:

39 ft

Length:

30 ft 11 in

Height:

11 ft 7 in

Wing Area:

242 sq ft

Empty:

4,640 lb

All-up:

6,750 lb

Max Speed:

240 mph at 5,800 ft

Climb:

8 min to 10,000 ft

Range:

694 miles

Preserved in British Museums

Martinet TT.1:

TF-SHC - Museum of Berkshire Aviation, Woodley - Restoration

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