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Ares I-X Flight Test Development Challenges and Success FactorsThe NASA Constellation Program's Ares I-X rocket launched successfully on October 28, 2009 collecting valuable data and providing risk reduction for the Ares I project. The Ares I-X mission was formulated and implemented in less than four years commencing with the Exploration Systems Architecture Study in 2005. The test configuration was founded upon assets and processes from other rocket programs including Space Shuttle, Atlas, and Peacekeeper. For example, the test vehicle's propulsion element was a Shuttle Solid Rocket Motor. The Ares I-X rocket comprised a motor assembly, mass and outer mold line simulators of the Ares I Upper Stage, Orion Spacecraft and Launch Abort System, a roll control system, avionics, and other miscellaneous components. The vehicle was 327 feet tall and weighed approximately 1,800,000 pounds. During flight the rocket reached a maximum speed of Mach 4.8 and an altitude of 150,000 feet. The vehicle demonstrated staging at 130,000 feet, tested parachutes for recovery of the motor, and utilized approximately 900 sensors for data collection. Developing a new launch system and preparing for a safe flight presented many challenges. Specific challenges included designing a system to withstand the environments, manufacturing large structures, and re-qualifying heritage hardware. These and other challenges, if not mitigated, may have resulted in test cancellation. Ares I-X succeeded because the mission was founded on carefully derived objectives, led by decisive and flexible management, implemented by an exceptionally talented and dedicated workforce, and supported by a thorough independent review team. Other major success factors include the use of proven heritage hardware, a robust System Integration Laboratory, multi-NASA center and contractor team, concurrent operations, efficient vehicle assembly, effective risk management, and decentralized element development with a centralized control board. Ares I-X was a technically complex test that required creative thinking, risk taking, and a passion to succeed.
Document ID
20110011063
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Askins, Bruce
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Davis, Steve
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Olsen, Ronald
(Miltec Corp. Huntsville, AL, United States)
Taylor, James
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
December 6, 2010
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M11-0064
M10-0686
Meeting Information
Meeting: JANNAF 40th SMBS/36th PEDCS/27th RNTS/25th SEPS Joint Subcommittee meetings
Location: Orlando, FL
Country: United States
Start Date: December 6, 2010
End Date: December 10, 2010
Sponsors: Department of the Air Force, Department of the Navy, NASA Headquarters, Department of the Army
Distribution Limits
Public
Copyright
Public Use Permitted.

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