Turbomeca Astazou
id:
turbomeca-astazou-310-3681635
title:
Turbomeca Astazou
text:
The Turbomeca Astazou is a highly successful series of turboprop and turboshaft engines, first run in 1957. The original version weighed 110 kg (243 lb) and developed 240 kW (320 shp) at 40,000 rpm. It was admitted for aviation service on May 29, 1961, after a 150-hour test run. The main developing engineer was G. Sporer. It was named after two summits of the Pyrenees. A simplified version was built by Agusta as the Turbomeca-Agusta TA.230.
brand slug:
wiki
category slug:
encyclopedia
description:
original url:
https://en.wikipedia.org/wiki/Turbomeca_Astazou
date created:
date modified:
2023-06-15T00:44:42Z
main entity:
{"identifier":"Q824609","url":"https://www.wikidata.org/entity/Q824609"}
image:
{"content_url":"https://upload.wikimedia.org/wikipedia/commons/f/f7/Turbomeca_astazou_II_AF.jpg","width":2268,"height":1512}
fields total:
13
integrity:
14