Back to Propulsion Systems

RS-68

The RS-68 is a single-chamber LOX/LH2 gas-generator engine developed for Delta IV Common Booster Cores. Its original production form generated more than 650,000 lbf of sea-level thrust and powered the Delta IV launch family; this canonical row remains retired and does not assert the distinct RS-68A upgrade.

RS-68
NASA/Stennis (RS-68 final engine acceptance test, S23-054) · NASA/Stennis official image; NASA material is generally not subject to U.S. copyright under NASA Images and Media Usage Guidelines; credit NASA and imply no endorsement. Context: https://www.nasa.gov/news-release/nasa-stennis-aerojet-rocketdyne-closes-historic-commercial-test-partnership/ · Source

Identity

Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
RS-68
Status
retired

Details

Description
The RS-68 is a single-chamber LOX/LH2 gas-generator engine developed for Delta IV Common Booster Cores. Its original production form generated more than 650,000 lbf of sea-level thrust and powered the Delta IV launch family; this canonical row remains retired and does not assert the distinct RS-68A upgrade.
Developers
Dry Mass Kg
6803.89
Family
First Flight Date
2002-11-20
Length M
5.2832
Manufacturers
Propellants
liquid hydrogenliquid 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

Assets & Meta

Creation Time
July 29, 2026 at 09:31:28 UTC
Updated Time
August 22, 2026 at 01:25:37 UTC

Other

Sources