{{Short description|1980s Czech turboprop aircraft engine}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{infobox aero engine |name= M602 |image= File:Walter M602 Prague 2017 01.jpg |caption= M602 on display at the Kbely Aviation Museum |engine_type= Turboprop |national_origin = Czechoslovakia |manufacturer= Walter Aircraft Engines |first_run= 25 February 1986<ref name=WJ2001>{{cite web |url= http://www.walterjinonice.cz/turbovrtulovy-motor-m602 |title= Turbovrtulový motor M602 |language= cs}}</ref> |major_applications= Let L-610 |number_built = |developed_from = |variants_with_their_own_articles = }}
The '''Walter M602''' is a turboprop aircraft engine produced by Walter Aircraft Engines of the Czechoslovakia, used on the Let L-610.
==Applications== * Let L-610
==Specification== {{jetspecs| <!-- If you do not understand how to use this template, please ask at Wikipedia talk:WikiProject Aircraft --> <!-- Please include units where appropriate (main comes first, alt in parentheses). If data are missing, leave the parameter blank (do not delete it). For additional lines, end your alt units with </li> and start a new, fully-formatted line with <li> --> |ref= ''Jane's All the World's Aircraft 2005–2006''<ref>{{cite book |title= Jane's All the World's Aircraft |date= 2005–2006 |page= 847}}</ref><ref name=FLIGHT28029024>{{cite journal|title=CREDITABLE COMMUTER|journal=Flight International|date=28 February 1990|pages=24–30|url=https://www.flightglobal.com/FlightPDFArchive/1990/1990%20-%200564.PDF|accessdate=14 December 2015}}</ref> |type=Three-spool turboprop engine |length=2565 mm (M602A), 2285 mm (M602B) |diameter=753 mm |weight=570 kg (M602A), 480 kg (M602B) |compressor=2-spool centrifugal compressor |combustion= Annular combustion chamber<ref name=WJ2001/> |turbine= 1-stage HP axial turbine (with internally cooled blades), 1-stage axial IP compressor, 2-stage LP axial power turbine |fueltype=Aviation kerosene |oilsystem=pressure spray |power={{convert|1360|kW|abbr=on}} (M602A), maximum continuous {{convert|1200|kW|abbr=on}},<ref name=WJ2001/> {{convert|1500|kW|abbr=on}} (M602B) |thrust= |compression=12<ref name=WJ2001/> |aircon= {{convert|7.33|kg/s|abbr=on}} |turbinetemp= 1388K<ref name=WJ2001/> |fuelcon= {{convert|0.330|kg/kWh|lb/hph|abbr=on}}<ref name=WJ2001/> |specfuelcon= |power/weight={{#expr:1360/570round2}} kW/kg (M602A), {{#expr:1500/480round2}} kW/kg (M602B) |thrust/weight= }}
==See also== {{Aircontent |related=
|similar engines=
|lists= * List of aircraft engines
|see also= }}
==References== {{Commons category}} {{Reflist}}
{{Walter aeroengines}}
Category:1980s turboprop engines M602