Pratt & Whitney J75-P-13
Pratt & Whitney J75-P-13 exact turbojet variant identified in U.S. Air Force technical-order material and the National Museum's U-2A record; this packet asserts propulsion identity only and does not infer a vehicle installation, actor attribution, or adjacent J75 variant.
Identity
- Aliases
- J75-P-13Pratt & Whitney J75-P-13J75 P-13
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbojet
- Name
- Pratt & Whitney J75-P-13
- Status
- unknown
Details
- Air Breathing Specs
- Afterburning Thrust Kn
- 75.6
- Description
- Pratt & Whitney J75-P-13 exact turbojet variant identified in U.S. Air Force technical-order material and the National Museum's U-2A record; this packet asserts propulsion identity only and does not infer a vehicle installation, actor attribution, or adjacent J75 variant.
Links
Assets & Meta
- Creation Time
- August 7, 2026 at 03:56:36 UTC
- Updated Time
- August 7, 2026 at 03:56:36 UTC
Other
- Sources
- Accessed Date
- 2026-08-06
- Note
- Official Air Force-hosted technical-order index explicitly identifies the J75-P-13/-17/-19 engine group and the U-2 application; this packet uses the exact P-13 identity without collapsing sibling suffixes.
- Publisher
- U.S. Air Force / Tinker Air Force Base
- Title
- NAVAIR 17-15-50.3 / T.O. 33-1-37-3 engine technical-order index
- Accessed Date
- 2026-08-06
- Note
- Official museum record distinguishes the U-2A's J57-P-37A from later U-2 models using J75-P-13; it supports exact variant identity but no vehicle relationship is written here.
- Publisher
- National Museum of the United States Air Force
- Title
- Lockheed U-2A