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RS-68A

RS-68A is the uprated, single-chamber LOX/LH2 gas-generator derivative of RS-68, developed for higher Delta IV Heavy performance. NASA records about 705,000 lbf (3,123 kN) thrust, first flight in June 2012, and three RS-68A engines on the Delta IV Heavy Common Booster Cores; status remains retired.

Identity

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

Details

Description
RS-68A is the uprated, single-chamber LOX/LH2 gas-generator derivative of RS-68, developed for higher Delta IV Heavy performance. NASA records about 705,000 lbf (3,123 kN) thrust, first flight in June 2012, and three RS-68A engines on the Delta IV Heavy Common Booster Cores; status remains retired.
Developers
Dry Mass Kg
6747.64
Family
First Flight Date
2012-06-29
Length M
5.1816
Lineage
Manufacturers
Propellants
liquid hydrogenliquid oxygen
Rocket Specs
Chamber Count
1
Cycle
gas generator
Sea Level Thrust Kn
3,137
Vacuum Specific Impulse S
411.9

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Creation Time
July 29, 2026 at 09:31:33 UTC
Updated Time
August 22, 2026 at 01:20:02 UTC

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