Armstrong Siddeley Python: Difference between revisions

Content deleted Content added
Cydebot (talk | contribs)
m Robot - Moving category Turboprop engines 1940–1949 to Category:1940s turboprop engines per CFD at Wikipedia:Categories for discussion/Log/2019 April 19.
Line 44:
|<!-- 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=''Flight''.<ref>[http://www.flightglobal.com/pdfarchive/view/1954/1954%20-%200979.html Flight Global Archive - 1954] www.flightglobal.com. Retrieved: 3 November 2008</ref>
|type=[[Turboprop]]
|length=123.2 in (3129313 mmcm)
|diameter=54 in (1372137 mmcm)
|weight=3,450 lb (15651,565 kg)
|compressor=axialAxial flow; 14 stages
|combustion=11 combustion chambers
|turbine=axialAxial flow; two stages
|fueltype=
|oilsystem=
Line 57:
|thrust=
|compression=5.35:1
|aircon=52.5 lb/s (23.8&nbsp; kg/s)
|turbinetemp=
|fuelcon=