Allison J33-A-35
Allison J33-A-35 is a historical centrifugal-flow turbojet variant. The National Museum of the United States Air Force identifies it as the J33-series engine used exclusively on the F-80C fighter, T-33A trainer, and Navy TV-2 trainer; Allison produced more than 6,600 from 1949 to 1955. Its normal thrust is 4,600 lb (20.461 kN, derived), rising to 5,400 lb (24.015 kN, derived) with water/alcohol injection. This exact variant remains separate from broader J33, aircraft, missile, and actor records.
Identity
- Aliases
- J33-A-35Allison J33-A-35J33
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbojet
- Name
- Allison J33-A-35
- Status
- historical
Details
- Air Breathing Specs
- Max Thrust Kn
- 20.461
- Description
- Allison J33-A-35 is a historical centrifugal-flow turbojet variant. The National Museum of the United States Air Force identifies it as the J33-series engine used exclusively on the F-80C fighter, T-33A trainer, and Navy TV-2 trainer; Allison produced more than 6,600 from 1949 to 1955. Its normal thrust is 4,600 lb (20.461 kN, derived), rising to 5,400 lb (24.015 kN, derived) with water/alcohol injection. This exact variant remains separate from broader J33, aircraft, missile, and actor records.
Links
Assets & Meta
- Creation Time
- August 7, 2026 at 04:39:28 UTC
- Updated Time
- August 21, 2026 at 09:10:00 UTC
Other
- Sources
- Accessed Date
- 2026-08-06
- Note
- Official museum fact sheet identifies the displayed J33-A-35 variant and records its 4,600 lb thrust and single-stage centrifugal/axial architecture.
- Publisher
- National Museum of the United States Air Force
- Title
- Allison J33 Turbojet