This Government Contract opportunity was posted on April 20, 2010. The submission period has ended. Browse the details below for market research, or find similar active opportunities.
RECOVERY -TILT ROTOR TEST RIG
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This contract pertains to the development and delivery of a Tilt Rotor Test Rig (TTR) for NASA’s Ames Research Center (ARC) under the Recovery Subsonic Rotary Wing Technology Development program. The task involves designing a rig capable of testing single rotors of approximately 25 feet in diameter in the 40x80 Foot Wind Tunnel and 40-foot diameter rotors in the 80x120 Foot Wind Tunnel. The TTR is designed to support various rotor operating modes including hover, edgewise, conversion, and airplane modes, enabled by wind tunnel turntable rotation to attain maximum airspeeds within each test section. The resulting capability is aimed at advancing next-generation vertical lift aircraft with improved performance and productivity. This opportunity is exclusively available to Bell Textron Helicopter Company under contract number NNA09DA55C and is funded through the American Recovery and Reinvestment Act of 2009. The task order will be fully funded via a contract modification and involves no solicitation for proposals, only informational notice. All communications and inquiries must be submitted in writing to the designated NASA contact. The work supports NASA’s Aeronautics Research Mission Directorate, reinforcing efforts to advance aeronautic technology under the Recovery Act.
General Info
Agency
Contract Value
$5,531,391Place of Performance
Not specifiedSet-Aside
Award Issued Date
Documents
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Timeline
Submission Closed
Organization & Contact Information
Full Description
Recovery Task Order 1, titled Tilt Rotor Test Rig Development, supports NASA Recovery Actwork sponsored by the Aeronautics Research Mission Directorate.
Bell is responsible for the design, development and delivery to NASA Ames Research Centera Tiltrotor Test Rig (TTR) for use at the NASA Ames Research Center (ARC) wind tunneltest facility. The TTR shall enable testing single, approximately 25-ft diameter rotors,in the 40 by 80 Foot Wind Tunnel and 40-ft diameter rotors in the 80 by 120 Foot WindTunnel. The TTR will enable rotor operation in hover, edgewise, conversion, and airplanemodes through wind tunnel turntable rotation, to the maximum airspeeds in each testsection. The result of this task will enable next generation vertical lift aircraft withsubstantial performance and productivity improvements.
This award notice is for INFORMATIONAL PURPOSES ONLY. The task order is issued under anexisting Cost Plus Fixed Fee contract NNA09DA55C, which was made on a competitive basis.Due to the nature of this work, a Cost Plus Fixed Fee task order was determinedappropriate.
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