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RS-68
The original gas-generator-cycle hydrogen engine developed for Delta IV's common booster core.
Identity
Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
RS-68
Status
retired
Details
Description
The original gas-generator-cycle hydrogen engine developed for Delta IV's common booster core.
Family
Family
Propellants
liquid hydrogen
liquid oxygen
Rocket Specs
Chamber Count
1
Cycle
gas generator
Sea Level Specific Impulse S
357
Sea Level Thrust Kn
2,949
Vacuum Specific Impulse S
409
Vacuum Thrust Kn
3,372
Links
Official Url
https://www.ulalaunch.com/docs/default-source/rockets/delta-iv-user%27s-guide.pdf
Assets & Meta
Creation Time
July 29, 2026 at 09:31:28 UTC
Updated Time
July 29, 2026 at 09:32:26 UTC
Other
Sources
Accessed Date
2026-07-29
Publisher
United Launch Alliance
Title
Final Delta IV Heavy launch
Url
https://newsroom.ulalaunch.com/releases/marking-the-end-of-an-era-united-launch-alliance-successfully-launches-final-delta-iv-heavy-rocket
Accessed Date
2026-07-29
Publisher
NASA Technical Reports Server
Title
Liquid Rocket Propulsion: RS-68 and Linear Aerospike
Url
https://ntrs.nasa.gov/citations/20000025317
Accessed Date
2026-07-29
Note
Supports the legacy vehicle installation and the narrow canonical identity used for migration.
Publisher
Official vehicle or program source
Title
Delta IV Medium official vehicle reference
Url
https://www.ulalaunch.com/docs/default-source/rockets/delta-iv-user%27s-guide.pdf
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