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Reusable Solid Rocket Motor - Accomplishment, Lessons, and a Culture of SuccessThe Reusable Solid Rocket Motor (RSRM) represents the largest solid rocket motor (SRM) ever flown and the only human-rated solid motor. High reliability of the RSRM has been the result of challenges addressed and lessons learned. Advancements have resulted by applying attention to process control, testing, and postflight through timely and thorough communication in dealing with all issues. A structured and disciplined approach was taken to identify and disposition all concerns. Careful consideration and application of alternate opinions was embraced. Focus was placed on process control, ground test programs, and postflight assessment. Process control is mandatory for an SRM, because an acceptance test of the delivered product is not feasible. The RSRM maintained both full-scale and subscale test articles, which enabled continuous improvement of design and evaluation of process control and material behavior. Additionally RSRM reliability was achieved through attention to detail in post flight assessment to observe any shift in performance. The postflight analysis and inspections provided invaluable reliability data as it enables observation of actual flight performance, most of which would not be available if the motors were not recovered. RSRM reusability offered unique opportunities to learn about the hardware. NASA is moving forward with the Space Launch System that incorporates propulsion systems that takes advantage of the heritage Shuttle and Ares solid motor programs. These unique challenges, features of the RSRM, materials and manufacturing issues, and design improvements will be discussed in the paper.
Document ID
20120002895
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Moore, D. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Phelps, W. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
December 5, 2011
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M11-1283
Report Number: M11-1283
Meeting Information
Meeting: JANNAF 6th Liquid Propulsion Subcommittee Meeting
Location: Hunsville, AL
Country: United States
Start Date: December 5, 2011
End Date: December 9, 2011
Sponsors: NASA Headquarters, Department of the Army, Department of the Air Force, Department of the Navy
Funding Number(s)
CONTRACT_GRANT: NAS8-9723
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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