TR-107
Historical Northrop Grumman TR-107 liquid-rocket-engine concept from NASA's Next Generation Launch Technology work. NASA identifies the TR-107 as an oxygen-rich staged-combustion LOX/RP-1 concept distinct from Boeing Rocketdyne's RS-84; no flight vehicle installation or unsupported performance figure is asserted here.
Identity
- Aliases
- TR-107Northrop Grumman TR-107
- Domains
- spaceflight
- Identity Level
- model
- Kind
- liquid-rocket-engine
- Name
- TR-107
- Status
- historical
Details
- Description
- Historical Northrop Grumman TR-107 liquid-rocket-engine concept from NASA's Next Generation Launch Technology work. NASA identifies the TR-107 as an oxygen-rich staged-combustion LOX/RP-1 concept distinct from Boeing Rocketdyne's RS-84; no flight vehicle installation or unsupported performance figure is asserted here.
- Developers
- Manufacturers
- Propellants
- liquid oxygenRP-1
- Rocket Specs
- Cycle
- oxygen-rich staged combustion
Links
Assets & Meta
- Creation Time
- August 14, 2026 at 23:48:58 UTC
- Updated Time
- August 14, 2026 at 23:48:58 UTC
Other
- Sources
- Accessed Date
- 2026-08-14
- Note
- NASA identifies TR-107 as a Northrop Grumman concept and distinguishes it from Boeing Rocketdyne's RS-84; both consume LOX/RP-1 in an oxygen-rich staged-combustion cycle.
- Publisher
- NASA Technical Reports Server
- Title
- Using CFD as a Rocket Injector Design Tool
- Accessed Date
- 2026-08-14
- Note
- NASA's NGLT injector-design work documents TR-107 as a distinct large-engine concept under Northrop Grumman support.
- Publisher
- NASA Technical Reports Server
- Title
- TR-107 and RS-84 Injector Design Support