A Centaur V inside ULA’s Decatur, Alabama factory. Photo: United Launch Alliance

NASA has formally awarded a sole-source contract to United Launch Alliance for the upper stage engines that will propel the Orion spacecraft toward the Moon on the Artemis IV and Artemis V missions. The contract was granted without open bidding, according to a Justification for Other Than Full and Open Competition (JOFOC) signed Thursday at Marshall Space Flight Center.

The document, signed March 6 by NASA Senior Procurement Executive Marvin Horne, confirms that ULA’s Vulcan Centaur V upper stage — the same stage that powers ULA’s commercial Vulcan rocket — will replace the long-planned Exploration Upper Stage, or EUS, which had been the intended powerhouse for the Block 1B configuration of the Space Launch System beginning with Artemis IV.

The EUS cancellation effectively means NASA is standardizing on the Block 1 SLS configuration through at least Artemis V, a significant restructuring of the agency’s lunar architecture.

Blue Origin’s New Glenn Upper Stage Was Assessed

The document assessed two candidates: ULA’s Centaur V and Blue Origin’s New Glenn Upper Stage. The NGUS was disqualified primarily on schedule and infrastructure grounds. NASA noted that while the New Glenn upper stage completed a demonstration flight in January 2025 and a second flight in November 2025, it remains in early development phases. Furthermore, NASA stated, adapting it for SLS would require relocating the Mobile Launcher 1 crew access arm, modifying umbilical systems, shortening the stage to clear the Vehicle Assembly Building’s height constraints, and then requalifying the modified vehicle through full-scale testing — a process NASA concluded would blow past the Artemis IV launch readiness window.

The Centaur, by contrast, has a heritage dating to the 1960s, and it shares many commonalities with the Interim Cryogenic Propulsion Stage (ICPS) it is replacing:

Centaur V / ICPS Commonalities
What Centaur V and ICPS Have In Common
Commonality Details
Main Engine Both use the RL-10, one of the most flight-proven upper stage engines in American spaceflight history.
Avionics (INCA) The Inertial Navigation and Control Assembly flies on both vehicles, carrying over flight-proven software and ground commanding architecture.
Emergency Detection System ULA’s crew abort detection system, flying on Artemis II and III, is shared heritage with the Centaur V.
Propellants Both burn LOX and LH2, allowing KSC’s existing ground propellant infrastructure to be used with minimal changes.
Mobile Launcher Interfaces Centaur V is compatible with ML-1’s existing umbilical connections, requiring no major launcher modifications.
Ground Support Systems KSC’s Exploration Ground Systems infrastructure and integration emulators developed for ICPS carry over to Centaur V.
Workforce & Facilities The same ULA teams in Denver and at Cape Canaveral that supported Artemis I–III transition directly to Centaur V work.
Orion & SLS Interfaces Shared avionics and software allow Centaur V to interface with Orion and SLS without redesigning proven cross-program integration.
Sources: NASA MSFC Justification for Other Than Full and Open Competition (JOFOC), ULA Vulcan Centaur V Upper Stage, March 2026

Under the planned contract, ULA would deliver two flight units and one flight spare, with the first stage required at Kennedy Space Center no later than nine months prior to the Artemis IV launch, currently targeted for early 2028, and the second no later than L-9 months ahead of Artemis V, planned for late 2028. The estimated period of performance is approximately six years, covering production, integration, and post-flight requirements. The contract value is redacted in the public version of the document.

Timeline and Scope

Under the planned contract, ULA would deliver two flight units and one flight spare, with the first stage required at Kennedy Space Center no later than nine months prior to the Artemis IV launch, currently targeted for early 2028, and the second no later than L-9 months ahead of Artemis V, planned for late 2028. The estimated period of performance is approximately six years, covering production, integration, and post-flight requirements. The contract value is redacted in the public version of the document.

Contract Document

Charles Boyer
Author: Charles Boyer

NASA kid from Cocoa Beach, FL, born of Project Apollo parents and family. I’m a writer and photographer sharing the story of spaceflight from the Eastern Range here in Florida.


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