Rolls-Royce Spey Mk 202
Rolls-Royce Spey Mk 202 historical low-bypass turbofan model under the canonical Spey family. Rolls-Royce Military Aero Engines records 20,500 lbf (91.2 kN) thrust with reheat for the military Mk 202; Rolls-Royce also records the 1970s transfer of Mk 202 production rights to China, establishing a distinct licensed-production and technology-lineage boundary. The exact FGR.2 Phantom installation is preserved; current lifecycle remains unknown.
Identity
- Aliases
- Spey Mk 202Spey MK202RB.163 Mk 202
- Domains
- aviation
- Identity Level
- model
- Kind
- turbofan
- Name
- Rolls-Royce Spey Mk 202
- Status
- unknown
Details
- Air Breathing Specs
- Max Thrust Kn
- 91.2
- Description
- Rolls-Royce Spey Mk 202 historical low-bypass turbofan model under the canonical Spey family. Rolls-Royce Military Aero Engines records 20,500 lbf (91.2 kN) thrust with reheat for the military Mk 202; Rolls-Royce also records the 1970s transfer of Mk 202 production rights to China, establishing a distinct licensed-production and technology-lineage boundary. The exact FGR.2 Phantom installation is preserved; current lifecycle remains unknown.
- Developers
- Family
- Manufacturers
Links
Assets & Meta
- Creation Time
- August 14, 2026 at 20:52:40 UTC
- Updated Time
- August 15, 2026 at 07:31:03 UTC
Other
- Sources
- Accessed Date
- 2026-08-14
- Note
- Rolls-Royce records that it transferred Spey MK202 production patent rights to China in the 1970s, establishing the exact model and licensed-production boundary.
- Publisher
- Rolls-Royce
- Title
- Rolls-Royce in China
- Accessed Date
- 2026-08-14
- Note
- The UK parliamentary report independently describes China's licensed manufacture of the Rolls-Royce Spey Mk 202 and the later Chinese derivative boundary; no exact aircraft relationship is asserted in this packet.
- Publisher
- UK Intelligence and Security Committee
- Title
- China report
- Accessed Date
- 2026-08-15
- Note
- Rolls-Royce Military Aero Engines' technical history identifies the military Spey Mk 202 as producing 20,500 lbf thrust with reheat and describes its development for RAF and Royal Navy Phantom aircraft.
- Publisher
- Rolls-Royce Military Aero Engines Ltd
- Title
- Development of the Rolls-Royce Military Spey Mk202 Engine