Upcoming RS-25 Engine Test Series Will Demonstrate Lower Cost Rocket Engine Components for NASA’s Artemis Program
Aerojet Rocketdyne is set to commence the Retrofit-2 test series at NASA's Stennis Space Center, starting January 28, 2021, to validate new components for the RS-25 engine. This series involves seven hot-fire tests lasting up to 500 seconds each, expected to conclude by June. The new hardware aims to reduce RS-25 costs by 30% through advanced design and manufacturing technologies. Key components include a HIP-bonded combustion chamber and additively manufactured Pogo assembly, enhancing efficiency and reliability in production.
- 30% cost reduction in RS-25 engine production.
- Advanced design techniques like Hot Isostatic Pressing (HIP) and additive manufacturing to improve efficiency.
- Seven hot-fire tests lasting up to 500 seconds to validate engine components.
- None.
STENNIS SPACE CENTER, Miss., Jan. 27, 2021 (GLOBE NEWSWIRE) -- Aerojet Rocketdyne and NASA are gearing up for a new phase of RS-25 hot-fire testing that will validate new components for the engine, which powers the core stage of the agency’s Space Launch System super heavy-lift exploration rocket.
The Retrofit-2 test series, consisting of seven tests at NASA’s Stennis Space Center, is expected to begin Jan. 28 and run through June. Each hot-fire test will last up to 500 seconds on the A1 Test Stand.
“This new hardware will significantly reduce the cost of the RS-25 rocket engine by leveraging important advances in design, materials and manufacturing technology,” said Eileen P. Drake, Aerojet Rocketdyne CEO and president.
Aerojet Rocketdyne is under contract to build 24 new engines, and the components being validated in this test series will be introduced in this production set. This new configuration will result in a
Some of the components being demonstrated in the Retrofit-2 series were featured on the previous Retrofit-1B test campaign. These include a combustion chamber built using a high-tech brazing technique called Hot Isostatic Pressing (HIP), and an additively manufactured Pogo Accumulator Assembly, a beach ball-sized component that damps out liquid oxygen system pressure oscillations.
This test series will put a second HIP-bonded main combustion chamber through a comprehensive series of tests. Aerojet Rocketdyne chose a HIP-bonded design because it eliminates difficult and time consuming plating processes, reduces welding defects and costly rework. Development and certification models of the HIP-bonded combustion chamber have been completed and six production units are being assembled at Aerojet Rocketdyne.
The Retrofit-2 series will also continue to test the same Pogo hardware that was previously tested to further verify its durability. The additively manufactured Pogo assembly has already been tested 13 times, accumulating 5,400 seconds of total firing time. The additively manufactured Pogo design eliminates more than 20 parts, more than 100 welds and reduces fabrication time by more than
Retrofit-2 also will test two RS-25 high pressure fuel and oxidizer turbopumps built from simplified designs using modern techniques as well as 3D printed valves and redesigned actuators.
About Aerojet Rocketdyne: Aerojet Rocketdyne, a subsidiary of Aerojet Rocketdyne Holdings, Inc. (NYSE:AJRD), is a world-recognized aerospace and defense leader that provides propulsion systems and energetics to the space, missile defense and strategic systems, and tactical systems areas, in support of domestic and international customers. For more information, visit www.Rocket.com and www.AerojetRocketdyne.com. Follow Aerojet Rocketdyne and CEO Eileen Drake on Twitter at @AerojetRdyne and @DrakeEileen.
Media Contacts:
Mary Engola, Aerojet Rocketdyne, 571-289-1371
Mary.Engola@rocket.com
Todd McConnell, Aerojet Rocketdyne, 561-882-5395
Todd.McConnell@rocket.com
FAQ
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