RL10C-2
RL10C derivative used by the SLS interim cryogenic propulsion stage for Artemis II and Artemis III.
Identity
- Domains
- spaceflight
- Identity Level
- variant
- Kind
- liquid-rocket-engine
- Name
- RL10C-2
- Status
- active
Details
- Description
- RL10C derivative used by the SLS interim cryogenic propulsion stage for Artemis II and Artemis III.
- Family
- Propellants
- liquid hydrogenliquid oxygen
- Rocket Specs
- Restartable
- Yes
- Vacuum Thrust Kn
- 110.1
Links
Assets & Meta
- Creation Time
- August 13, 2026 at 20:52:56 UTC
- Updated Time
- August 13, 2026 at 20:52:56 UTC
Other
- Sources
- Accessed Date
- 2026-08-13
- Publisher
- NASA
- Title
- Space Launch System RL10 Engine
- Accessed Date
- 2026-08-13
- Publisher
- NASA
- Title
- Artemis II Reference Guide
- Accessed Date
- 2026-08-13
- Publisher
- NASA
- Title
- Space Launch System