SNECMA Atar 9K50
Exact SNECMA Atar 9K50 afterburning turbojet variant. Dassault documents the engine in Mirage G4/G8 development and Mirage 50 service; French aviation-heritage documentation records its 1969 certification, 1973 Mirage F1 production entry, and distinct 9K50 design boundary. This packet creates propulsion identity only and asserts no family link, actor attribution, Mirage installation, sibling mutation, or lineage edge.
Identity
- Aliases
- Atar 9K50ATAR 09K50SNECMA ATAR 9K50
- Domains
- aviation
- Identity Level
- variant
- Kind
- turbojet
- Name
- SNECMA Atar 9K50
- Status
- historical
Details
- Air Breathing Specs
- Afterburning Thrust Kn
- 70.6
- Description
- Exact SNECMA Atar 9K50 afterburning turbojet variant. Dassault documents the engine in Mirage G4/G8 development and Mirage 50 service; French aviation-heritage documentation records its 1969 certification, 1973 Mirage F1 production entry, and distinct 9K50 design boundary. This packet creates propulsion identity only and asserts no family link, actor attribution, Mirage installation, sibling mutation, or lineage edge.
Links
Assets & Meta
- Creation Time
- August 7, 2026 at 06:22:54 UTC
- Updated Time
- August 7, 2026 at 06:22:54 UTC
Other
- Sources
- Accessed Date
- 2026-08-07
- Note
- Official Dassault history identifies the Snecma Atar 9K 50 as the Mirage 50 engine and distinguishes that model from the Mirage III/5 family context.
- Publisher
- Dassault Aviation
- Title
- Mirage 50: origins, characteristics and performance data
- Accessed Date
- 2026-08-07
- Note
- Official Dassault history identifies twin Atar 9 K 50 engines for the Mirage G4 prototypes and Atar 9 K 50 on Mirage G8 02, proving the exact variant designation.
- Publisher
- Dassault Aviation
- Title
- Mirage G: origins, characteristics and performance
- Accessed Date
- 2026-08-07
- Note
- Aviation-heritage technical record identifies the 09K50 as a reheated axial turbojet, records October 1969 certification, 1973 Mirage F1 production entry, and 7,060 daN afterburning thrust; the suffix is kept distinct from 9C/9K.
- Publisher
- Conservatoire d'Aéronautique d'Aquitaine
- Title
- Turboréacteur SNECMA ATAR 09K50