A single-spool afterburning turbojet with distinctive high-speed compressor-bleed bypass operation.
NASA Photo / Tony Landis · NASA states its content generally is not subject to U.S. copyright when not identified as third-party material, subject to NASA media-usage guidelines; use factually, credit NASA Photo / Tony Landis, do not imply NASA endorsement, and do not treat NASA identifiers or logos as freely reusable. The NASA page identifies this image as NASA Photo / Tony Landis rather than a third-party licensed work. · Source
Identity
Aliases
JT11D-20
Domains
aviation
Identity Level
model
Kind
turbojet
Name
Pratt & Whitney J58
Status
retired
Details
Air Breathing Specs
Afterburning Thrust Kn
133.44
Spool Count
1
Description
A single-spool afterburning turbojet with distinctive high-speed compressor-bleed bypass operation.
Smithsonian's exact J58/JT11D-20 collection record lists 133,440 N afterburning thrust, an 8-stage axial compressor, a 2-stage turbine, and afterburner configuration; thrust is normalized to 133.44 kN.