Pratt & Whitney J58 turbojet
GPTKB entity
Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:constructionStartYear |
1956
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
4 ft 2 in (1.27 m)
|
| gptkbp:firstFlight |
1963
|
| gptkbp:fuelType |
gptkb:JP-7
|
| gptkbp:length |
17 ft 10 in (5.44 m)
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:maximumSpeed |
Mach 3.2
|
| gptkbp:notableFeature |
bleed bypass system
continuous afterburner operation designed for sustained supersonic flight |
| gptkbp:numberOfStages |
2
9 |
| gptkbp:operationalCeiling |
85,000 ft
|
| gptkbp:retired |
1998
|
| gptkbp:thrust |
34,000 lbf
32,500 lbf (dry) |
| gptkbp:type |
afterburning turbojet
|
| gptkbp:usedIn |
gptkb:aircraft
gptkb:Lockheed_A-12 gptkb:Lockheed_YF-12 |
| gptkbp:weight |
6,000 lb (2,722 kg)
|
| gptkbp:bfsParent |
gptkb:Blackbird_(jet)
gptkb:A-12_Oxcart_spy_plane |
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney J58 turbojet
|