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Development of the Functional Flow Block Diagram for the J-2X Rocket Engine SystemThe J-2X program calls for the upgrade of the Apollo-era Rocketdyne J-2 engine to higher power levels, using new materials and manufacturing techniques, and with more restrictive safety and reliability requirements than prior human-rated engines in NASA history. Such requirements demand a comprehensive systems engineering effort to ensure success. Pratt & Whitney Rocketdyne system engineers performed a functional analysis of the engine to establish the functional architecture. J-2X functions were captured in six major operational blocks. Each block was divided into sub-blocks or states. In each sub-block, functions necessary to perform each state were determined. A functional engine schematic consistent with the fidelity of the system model was defined for this analysis. The blocks, sub-blocks, and functions were sequentially numbered to differentiate the states in which the function were performed and to indicate the sequence of events. The Engine System was functionally partitioned, to provide separate and unique functional operators. Establishing unique functional operators as work output of the System Architecture process is novel in Liquid Propulsion Engine design. Each functional operator was described such that its unique functionality was identified. The decomposed functions were then allocated to the functional operators both of which were the inputs to the subsystem or component performance specifications. PWR also used a novel approach to identify and map the engine functional requirements to customer-specified functions. The final result was a comprehensive Functional Flow Block Diagram (FFBD) for the J-2X Engine System, decomposed to the component level and mapped to all functional requirements. This FFBD greatly facilitates component specification development, providing a well-defined trade space for functional trades at the subsystem and component level. It also provides a framework for function-based failure modes and effects analysis (FMEA), and a rigorous baseline for the functional architecture.
Document ID
20070031871
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
White, Thomas
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Stoller, Sandra L.
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Greene, WIlliam D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Christenson, Rick L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bowen, Barry C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
May 14, 2007
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: JANNAF Interagency Propulsion Conference
Location: Denver, CO
Country: United States
Start Date: May 14, 2007
End Date: May 17, 2007
Funding Number(s)
CONTRACT_GRANT: NNM06AB13C
Distribution Limits
Public
Copyright
Other

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