The General Electric J73 turbojet was developed by General Electric from the earlier J47 engine. Its original USAF designation was J47-21, but the innovative features (variable inlet guide vanes, and single-shell combustor case) led to its redesignation as J73.
Attributes | Values |
---|---|
rdf:type | |
rdfs:label |
|
rdfs:comment |
|
sameAs | |
combustion |
|
Developed Into | |
Length |
|
dcterms:subject | |
dbkwik:military/pr...iPageUsesTemplate | |
diameter |
|
Type |
|
Unit Cost |
|
major applications | |
Weight |
|
Thrust |
|
Manufacturer |
|
aircon |
|
thrust/weight |
|
National Origin | |
Developed From | |
specfuelcon |
|
compression |
|
turbine |
|
Number Built |
|
compressor |
|
ref |
|
abstract |
|
is Developed From of |