About: Snecma M53   Sponge Permalink

An Entity of Type : dbkwik:resource/t0EYzM3e0H-TCd0voM-X1Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The SNECMA M53 is an afterburning turbofan engine developed for the Dassault Mirage 2000 fighter by Snecma. The engine is in service with different air forces, including the latest Mirage 2000-5 and 2000-9 multirole fighters.

AttributesValues
rdf:type
rdfs:label
  • Snecma M53
rdfs:comment
  • The SNECMA M53 is an afterburning turbofan engine developed for the Dassault Mirage 2000 fighter by Snecma. The engine is in service with different air forces, including the latest Mirage 2000-5 and 2000-9 multirole fighters.
sameAs
combustion
  • annular
Length
  • 5070.0
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
diameter
  • 796(xsd:integer)
Type
  • Turbofan
  • Afterburning single-shaft turbofan
bypass
  • 0(xsd:double)
major applications
Weight
  • 1515.0
Thrust
  • *64 kN military thrust *95 kN with afterburner
Manufacturer
thrust/weight
  • 6(xsd:double)
National Origin
  • France
specfuelcon
  • *0.90 Dry engine thrust *2.10 military thrust
compression
  • 9(xsd:double)
turbine
  • 2(xsd:integer)
compressor
  • 8(xsd:integer)
abstract
  • The SNECMA M53 is an afterburning turbofan engine developed for the Dassault Mirage 2000 fighter by Snecma. The engine is in service with different air forces, including the latest Mirage 2000-5 and 2000-9 multirole fighters.
Alternative Linked Data Views: ODE     Raw Data in: CXML | CSV | RDF ( N-Triples N3/Turtle JSON XML ) | OData ( Atom JSON ) | Microdata ( JSON HTML) | JSON-LD    About   
This material is Open Knowledge   W3C Semantic Web Technology [RDF Data] Valid XHTML + RDFa
OpenLink Virtuoso version 07.20.3217, on Linux (x86_64-pc-linux-gnu), Standard Edition
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2012 OpenLink Software