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Update on Risk Reduction Activities for a Liquid Advanced Booster for NASA's Space Launch SystemDynetics has designed innovative structure assemblies; manufactured them using Friction Stir Welding (FSW) to leverage NASA investments in tools, facilities, and processes; conducted proof and burst testing, demonstrating viability of design/build processes Dynetics/AR has applied state-of-the-art manufacturing and processing techniques to the heritage F-1, reducing risk for engine development Dynetics/AR has also made progress on technology demonstrations for ORSC cycle engine, which offers affordability and performance for both NASA and other launch vehicles Full-scale integrated oxidizer-rich test article. Testing will evaluate performance and combustion stability characteristics. Contributes to technology maturation for ox-rich staged combustion engines.
Document ID
20160012069
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Crocker, Andy (Dynetics, Inc. Huntsville, AL, United States)
Graham, Bart (Aerojet-General Corp. Huntsville, AL, United States)
Date Acquired
October 7, 2016
Publication Date
September 26, 2016
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M16-5553
Meeting Information
Meeting: International Astronautical Congress
Location: Guadalajara
Country: Mexico
Start Date: September 26, 2016
End Date: September 30, 2016
Sponsors: International Astronautical Federation
Funding Number(s)
CONTRACT_GRANT: NNM12AA67C
Distribution Limits
Public
Copyright
Public Use Permitted.

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