- Miles Hawk Trainer
infobox Aircraft
name = Hawk Trainer
type = Two-seat touring and racing monoplane
manufacturer = Miles Aircraft Limited
caption =
designer =Frederick George Miles
first flight = 1935
introduced =
retired =
status =
primary user =Royal Air Force
more users =Romanian Air Force
produced =
number built = 27
unit cost =
developed from =Miles Hawk Major
variants with their own articles =Miles Magister The Miles Hawk Trainer was a 1930s British two-seat training monoplane designed by Miles Aircraft Limited.
Design and development
The
Miles Hawk Trainer was developed from the Hawk Major to meet a requirement to supplement thede Havilland Tiger Moth in the training role. The aircraft had dual controls, blind flying equipment and vacuum operated flaps. In 1937 the design was further developed to meet an Air Ministry specification for a trainer and became the M.14 Magister.Variants
;M.2W Hawk Trainer:Initial production version powered buy a
de Havilland Gipsy Major engine, four built.;M.2X Hawk Trainer:Improved version with a larger horn-balanced rudder, nine built.;M.2Y Hawk Trainer:M.2X with minor changes, 13 built.
*Note that Hawk Trainer Mk II and Mk III were variants of theMiles Magister .Operators
;ROM
*Romanian Air Force ;UK
*Royal Air Force urvivors
*M.2W registered G-ADWT is still flyable and based in
England pecifications (M.2W)
aerospecs
met or eng?= engcrew=
capacity=Two
length m=
length ft=24
length in=0
span m=
span ft=34
span in=0
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=
height ft=6
height in=8
wing area sqm=
wing area sqft=176
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=1,210
gross weight kg=
gross weight lb=1,720
lift kg=
lift lb=eng1 number=1
eng1 type=de Havilland Gipsy Major
eng1 kw=
eng1 hp= 130
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=max speed kmh=241
max speed mph=150
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=644
range miles=400
endurance h=
endurance min=
ceiling m=5,486
ceiling ft=18,000
glide ratio=
climb rate ms=
climb rate ftmin=1,300
sink rate ms=
sink rate ftmin=armament1=
armament2=
armament3=
armament4=
armament5=
armament6=References
* Amos, Peter. and Brown, Don Lambert. "Miles Aircraft Since 1925, Volume 1". London: Putnam Aeronautical, 2000. ISBN 0-85177-787-0.
* Brown, Don Lambert. "Miles Aircraft Since 1925". London: Putnam & Company Ltd., 1970. ISBN 0-37000-127-3.
*cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=
*cite book |last= Jackson|first= A.J.|authorlink= |coauthors= |title= British Civil Aircraft since 1919 Volume 3|year= 1974|publisher= Putnam|location= London|isbn=0 370 10014 XExternal links
ee also
aircontent
related=
similar aircraft=
sequence=
lists=
*List of aircraft of the RAF
see also=
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