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System Engineering on the Use for Ares I,V - the Simpler, the BetterThe Ares I and Ares V Vehicles will utilize the J-2X rocket engine developed for NASA by the Pratt & Whitney Rocketdyne Company. The J-2X is an improved higher power version of the original J-2 engine used during the Apollo program. With higher power and updated requirements for safety and performance, the J-2X becomes a new engine using state-of-the-art design methodology, materials and manufacturing processes. The implementation of Systems Engineering (SE) principles enables the rapid J-2X development program to remain aligned with the ARES I and V vehicle programs, Meeting the aggressive development schedule is a challenge. Coordinating the best expertise thai NASA and PWR have to offer requires effectively utilizing resources at multiple sites. This presents formidable communication challenges. SE allows honest and open discussions of issues and problems. This simple idea is often overlooked in large and complex SE programs. Regular and effective meetings linking SE objectives to component designs are used to voice differences of opinions with customer and contractor in attendance so that the best mutual decisions can be made on the shortest possible schedule. Regular technical interchange meetings on secure program wide computer networks and CM processes are effective,in the "Controlled Change" process that exemplifies good SE. Good communication is a key effective SE implementation. The System of Systems approach is the vision of the Orion program which facilitates the establishment of dynamic SE processes at all levels including the engine. SE enables requirements evolution by facilitating organizational and process agility. Flow down and distribution of requirements is controlled by Allocation Reports which breakdown numerical design objectives (weight, reliability, etc.) into quanta goals for each component area. Linked databases of design and verification requirements helps eliminate redundancy and potential mistakes inherent m separated systems. Another tool, the Architecture Design Description, is being used to control J-2X system architecture and effectively communicate configuration changes to those involved in the design process. But the proof is in successful program accomplishment. The SE is the methodology being used to meet the challenge of completing J-2X engine certification 2 years ahead of any engine program ever developed at PWR. The Ares I SE system of systems has delivered according to expectations thus far. All major design reviews (SRR. PDR, CDR) have been successfully conducted to satisfy overall program objectives using SE as the basis for accomplishment. The paper describes SE tools and techniques utilized to achieve this success.
Document ID
20090008514
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Kelly, William
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Greene, William D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Greasley, Paul
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Ackerman, Peter C.
(Pratt and Whitney Rocketdyne Canoga Park, CA, United States)
Date Acquired
August 24, 2013
Publication Date
September 27, 2008
Subject Category
Systems Analysis And Operations Research
Report/Patent Number
MSFC-2017
Meeting Information
Meeting: 59th International Astronautical Congress
Location: Glasgow
Country: United Kingdom
Start Date: September 29, 2008
End Date: October 3, 2008
Sponsors: British Interplanetary Society
Funding Number(s)
CONTRACT_GRANT: NNM06AB13C
Distribution Limits
Public
Copyright
Other

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