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Universal Stage Adapter

Space Launch System/Universal Stage Adapter

NASA’s SLS (Space Launch System) rocket is designed to be flexible and evolvable to meet the mission needs of the Artemis campaign. With the Block 1B upgrade, which adds an Exploration Upper Stage (EUS) to increase the payload capability, the rocket requires a new adapter to connect it to the Orion spacecraft. 

A Universal Stage Adapter (USA) was envisioned to not only provide the structural connection but also enable a co-manifested payload to be delivered to orbit. The adapter protects the payload from initial encapsulation and stacking onto the SLS rocket through integration, system checkout, processing, rollout to the pad, and finally through launch and ascent. Once on orbit, the adapter carefully separates from the Exploration Upper Stage to allow the Orion capsule to dock with the payload and journey on to the Moon.

These photos and videos show how crews guided a test version of the universal stage adapter for NASA’s more powerful version of its SLS (Space Launch System) rocket to Building 4619 at the agency’s Marshall Space Flight Center in Huntsville, Alabama, Feb. 22. Built by Leidos, the lead contractor for the universal stage adapter, crews transported the hardware from a Leidos facility in Decatur, Alabama, the same day. The universal stage adapter will connect the SLS rocket’s upgraded in-space propulsion stage, called the exploration upper stage, to NASA’s Orion spacecraft as part of the evolved Block 1B configuration of the SLS rocket. It will also serve as a compartment capable of accommodating large payloads, such as modules or other exploration spacecraft.  In Building 4619’s Load Test Annex High Bay at Marshall, the development test article will first undergo modal testing that will shake the hardware to validate dynamic models. Later, during ultimate load testing, force will be applied vertically and to the sides of the hardware. Unlike the flight hardware, the development test article has flaws intentionally included in its design, which will help engineers verity that the flight adapter can withstand the extreme forces it will face during launch and flight.
These photos and videos show how crews guided a test version of the universal stage adapter for NASA’s more powerful version of its SLS (Space Launch System) rocket to Building 4619 at the agency’s Marshall Space Flight Center in Huntsville, Alabama, Feb. 22.
NASA/Brandon Hancock

NASA’s Glenn Research Center in Cleveland is leading the design and development of the Universal Stage Adapter on behalf of the SLS Program for the agency. The adapter will connect the Orion spacecraft to the SLS Exploration Upper Stage when it launches astronauts on the Block 1B Artemis IV mission. 

The Universal Stage Adapter leverages the latest in advanced composite materials to be as light as possible. Every pound of structure is equivalent to a pound of payload because the adapter is carried through the Exploration Upper Stage trans-lunar injection burn that will send Orion to the Moon. The adapter will be the largest fully composite human-rated primary structure ever flown and will maximize the payload mass capability for future Artemis missions.

The Universal Stage Adapter will be made of four composite honeycomb-core panels, with access doors, a separation system, a Vehicle Damping System (VDS) connection to help stabilize the vehicle on the mobile launcher, and a purge umbilical with disconnect to maintain a clean air internal environment before launch. At liftoff, the adapter will weigh less than 9,650 pounds. 

Expertise from across NASA was used to minimize the risk of the design and development of the new structures. This included the help of engineers not only at Glenn, but at NASA’s Langley Research Center in Hampton, Virginia, and NASA’s Marshall Space Flight Center in Huntsville, Alabama, to realize the design of the adapter. 

The Universal Stage Adapter is cone shaped with a cylindrical lower barrel. It is 18.0 feet in diameter on the Orion end (forward end), 27.6 feet in diameter at the Exploration Upper Stage end (aft end), and stands 33.1 feet tall. It will provide environmental control to payloads during ground operations and launch and ascent, and it will provide electrical and communication paths between SLS’s Exploration Upper Stage and Orion. 

The upgraded configuration of SLS, known as Block 1B, is the first use of the Universal Stage Adapter. It is managed by the SLS Spacecraft and Payload Integration and Evolution Office at NASA Marshall and will support Artemis IV and future missions. 

With the Exploration Upper Stage, which will be powered by four RL10-C3 engines, SLS will be capable of lifting more than 105 metric tons (231,000 pounds) from Earth’s surface. Unlike the previous Block 1 adapter, the Universal Stage Adapter will be capable of carrying large co-manifested payloads, such as a habitat. To protect and deploy those payloads, the design incorporates systems to control temperature, mitigate the acoustic environment, and safely separate without recontact to enable release of the payload. 

The Universal Stage Adapter is used for NASA’s SLS. The SLS is a powerful, advanced heavy-lift launch vehicle designed to be flexible and evolvable for deep-space destinations. The base contract effort, led by Dynetics (a subsidiary of Leidos), is to design, test, manufacture, and deliver one Universal Stage Adapter.  The acquisition also includes qualification and flight quick disconnects, payload encapsulation tooling, lifting Ground Support Equipment (GSE), transportation hardware, and ground processing and transportation cover.

Expanded view diagram of the SLS (Space Launch System) Block 1B rocket crew configuration illustrating discrete rocket components and their location within the stacked rocket. Indicated, from bottom to top, are call-outs for the four RS-25 engines, two solid rocket boosters to either side of the core stage, interstage, exploration upper stage (EUS) with its four RL-10 engines, payload adapter (PLA), co-manifested payload (exemplified for this illustration with a rendering of Lunar I-Hab) below the universal stage adapter (USA), and finally the Orion spacecraft with its spacecraft adapter, encapsulated service model panels, service module, crew module, and launch abort system.
Expanded view diagram of the SLS (Space Launch System) Block 1B rocket crew configuration illustrating discrete rocket components and their location within the stacked rocket. Indicated, from bottom to top, are call-outs for the four RS-25 engines, two solid rocket boosters to either side of the core stage, interstage, exploration upper stage (EUS) with its four RL-10 engines, payload adapter (PLA), co-manifested payload (exemplified for this illustration with a rendering of Lunar I-Hab) below the universal stage adapter (USA), and finally the Orion spacecraft with its spacecraft adapter, encapsulated service model panels, service module, crew module, and launch abort system.
NASA
Notional SLS Block 1B Crewed Configuration Vehicle
Notional SLS Block 1B Crewed Configuration Vehicle

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