Stock Markets January 27, 2026

Northrop Grumman’s Five-Segment Boosters to Drive Artemis II SLS Launch

Twin solid rocket motors to supply the majority of liftoff thrust for NASA’s first crewed deep-space mission since Apollo

By Priya Menon NOC
Northrop Grumman’s Five-Segment Boosters to Drive Artemis II SLS Launch
NOC

Northrop Grumman will provide the twin five-segment solid rocket boosters that will power NASA’s Space Launch System for the Artemis II crewed lunar flyby, with a launch window opening as early as February 6, 2026. The boosters, evolved from Shuttle-era hardware and validated on Artemis I, will deliver the lion’s share of the rocket’s thrust and include critical safety motors for the mission’s Launch Abort System.

Key Points

  • Northrop Grumman’s twin five-segment solid rocket boosters will power NASA’s Artemis II SLS launch, scheduled as early as February 6, 2026.
  • Each booster stands 177 feet tall and generates 3.6 million pounds of thrust; together they supply 7.2 million of the SLS’s 8.8 million pounds of launch thrust, more than 75 percent of total liftoff thrust.
  • Northrop Grumman is also manufacturing the attitude control motor and abort motor for the Launch Abort System, and continues work on the Gateway HAB/Logistics Outpost and next-generation boosters.

Northrop Grumman (NYSE:NOC) is set to supply the twin five-segment solid rocket boosters that will propel NASA’s Space Launch System (SLS) on the Artemis II mission, the agency’s first crewed voyage beyond the Moon since the Apollo era. The launch is scheduled to occur as early as February 6, 2026, from Pad 39B at Kennedy Space Center.

Each of the two boosters stands 177 feet tall and produces 3.6 million pounds of thrust. Combined, the pair will generate 7.2 million pounds of thrust at liftoff, accounting for more than 75 percent of the SLS rocket’s total launch thrust of 8.8 million pounds.

"We’ve leveraged our unparalleled manufacturing and solid rocket motor expertise to supply the SLS rocket with 7.2 million pounds of its 8.8 million pounds of total thrust at launch," said Jim Kalberer, vice president of propulsion systems at Northrop Grumman.

The five-segment configuration used for Artemis II is an evolution of the four-segment boosters that were flown on the Space Shuttle. That earlier architecture was also the basis for the hardware that performed on the Artemis I uncrewed test flight, providing a development lineage for the current motors.

In addition to the main boosters, Northrop Grumman is producing key safety propulsion elements for the mission's Launch Abort System (LAS). Those components include the attitude control motor and the abort motor, both designed to move the Orion spacecraft away from the rocket in the event of an emergency during ascent.

Artemis II will carry a four-person crew on an approximately 10-day mission that will travel around the Moon. The flight is intended to validate systems and hardware in a crewed deep-space environment as part of preparations for subsequent lunar operations and eventual missions to Mars.

Beyond supplying the boosters and LAS motors for Artemis II, Northrop Grumman remains engaged with the broader Artemis program. The company is working on the Habitat and Logistics Outpost module for the lunar Gateway station and continuing development of next-generation solid rocket boosters intended for future deep-space exploration.


Context and technical highlights

  • The twin boosters are the largest solid rocket motors ever used for human spaceflight by size and thrust.
  • They represent an upgrade from the four-segment Shuttle-era design and drew on validation from the Artemis I mission.
  • Northrop Grumman’s scope for Artemis includes both primary propulsion and crew safety motors, plus ongoing contributions to Gateway hardware and future booster development.

Risks

  • Launch timing is indicated as "as early as February 6, 2026," reflecting schedule uncertainty for the Artemis II mission and associated supplier and program timelines - impacts aerospace and launch-services sectors.
  • Artemis II is designed to confirm systems and hardware in crewed deep space, indicating that mission validation remains necessary before follow-on lunar and Mars exploration – affects spacecraft systems and mission-integration stakeholders.
  • Continued development work on the Gateway module and next-generation boosters implies ongoing technical and programmatic challenges that could affect contractors, supply chains, and program schedules in the aerospace sector.

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