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During the Artemis I uncrewed test flight, a single liquid hydrogen and liquid oxygen-fed
RL10B-2 engine producing 24,750 pounds (110kN) of thrust will serve as the main propulsion
for the Interim Cryogenic Propulsion Stage (ICPS) that will send the Orion spacecraft to the
Moon.
The rocket engine was developed by Pratt & Whitney in the late 1950s and was first
flown in 1963. Since then, more than 500 RL10 engines have flown to space. The RL10 is
manufactured by Space Launch System (SLS) lead contractor Aerojet Rocketdyne in West
Palm Beach, FL, and they have provided upper stage propulsion to launch hundreds of
satellites and have sent spacecraft to explore every planet in the solar system. With Artemis,
an updated version of the RL10 will send people farther away from Earth than humans have
ever traveled.
The first three Artemis missions will include an ICPS single RL10 configuration atop the SLS
Block 1 rocket. As the rocket evolves to a more powerful Block 1B configuration, it will fly with
the Exploration Upper Stage (EUS) that will use four RL10C-3 engines to send Orion and
large cargos to the Moon. The four RL10 engines on EUS provide more than 97,000 pounds
(431kN) of thrust, which will allow the rocket to send 40 percent more mass to the Moon.
Space Launch System
RL10 Engine
Proven, Reliable Space Propulsion
National Aeronautics and Space Administration
NASA
facts
A single RL10 engine will provide nearly 25,000 pounds of
thrust and serve as the main propulsion for the ICPS that
will fly atop the SLS rocket Block 1 in support of each of the
first three Artemis missions.
The Space Launch System ICPS mates with the launch
vehicle stage adapter atop the SLS core stage in the
Vehicle Assembly Building at NASA’s Kennedy Space
Center in Florida. The ICPS will fire its RL10 engine to send
the Orion spacecraft to the Moon.
National Aeronautics and Space Administration
George C. Marshall Space Flight Center
Huntsville, AL 35812
www.nasa.gov/marshall
www.nasa.gov
For more information about SLS, visit:
http://www.nasa.gov/artemis
http://www.nasa.gov/sls
http://www.twitter.com/NASA_SLS
http://www.facebook.com/NASASLS
http://www.instagram.com/exploreNASA
Launch Abort System
Crew Module
Service Module
Encapsulated Service Module Panels
Spacecraft Adapter
Orion Stage Adapter
Interim Cryogenic Propulsion Stage
RL10 Engine
Launch Vehicle Stage Adapter
Core Stage
Orion Multi-Purpose
Crew Vehicle
Solid Rocket Booster (2)
RS-25
Engine (4)
SLS Block 1
SLS Block 1 - Expanded View
NASA Facts
FS-2022-01-59-MSFC

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RL10 Engine

  • 1. During the Artemis I uncrewed test flight, a single liquid hydrogen and liquid oxygen-fed RL10B-2 engine producing 24,750 pounds (110kN) of thrust will serve as the main propulsion for the Interim Cryogenic Propulsion Stage (ICPS) that will send the Orion spacecraft to the Moon. The rocket engine was developed by Pratt & Whitney in the late 1950s and was first flown in 1963. Since then, more than 500 RL10 engines have flown to space. The RL10 is manufactured by Space Launch System (SLS) lead contractor Aerojet Rocketdyne in West Palm Beach, FL, and they have provided upper stage propulsion to launch hundreds of satellites and have sent spacecraft to explore every planet in the solar system. With Artemis, an updated version of the RL10 will send people farther away from Earth than humans have ever traveled. The first three Artemis missions will include an ICPS single RL10 configuration atop the SLS Block 1 rocket. As the rocket evolves to a more powerful Block 1B configuration, it will fly with the Exploration Upper Stage (EUS) that will use four RL10C-3 engines to send Orion and large cargos to the Moon. The four RL10 engines on EUS provide more than 97,000 pounds (431kN) of thrust, which will allow the rocket to send 40 percent more mass to the Moon. Space Launch System RL10 Engine Proven, Reliable Space Propulsion National Aeronautics and Space Administration NASA facts A single RL10 engine will provide nearly 25,000 pounds of thrust and serve as the main propulsion for the ICPS that will fly atop the SLS rocket Block 1 in support of each of the first three Artemis missions. The Space Launch System ICPS mates with the launch vehicle stage adapter atop the SLS core stage in the Vehicle Assembly Building at NASA’s Kennedy Space Center in Florida. The ICPS will fire its RL10 engine to send the Orion spacecraft to the Moon.
  • 2. National Aeronautics and Space Administration George C. Marshall Space Flight Center Huntsville, AL 35812 www.nasa.gov/marshall www.nasa.gov For more information about SLS, visit: http://www.nasa.gov/artemis http://www.nasa.gov/sls http://www.twitter.com/NASA_SLS http://www.facebook.com/NASASLS http://www.instagram.com/exploreNASA Launch Abort System Crew Module Service Module Encapsulated Service Module Panels Spacecraft Adapter Orion Stage Adapter Interim Cryogenic Propulsion Stage RL10 Engine Launch Vehicle Stage Adapter Core Stage Orion Multi-Purpose Crew Vehicle Solid Rocket Booster (2) RS-25 Engine (4) SLS Block 1 SLS Block 1 - Expanded View NASA Facts FS-2022-01-59-MSFC