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Giving Bigger Satellites a BoostUltramet, Inc. has spurred a new process for producing rocket engine thrust chambers, through SBIR funding and the Glenn Research Center. High-temperature oxidation-resistant thruster materials are being produced in order to achieve high-temperature capability without sacrificing reliability. These thruster materials lead to an estimated three-percent improvement in propulsion system performance. To develop this material, Ultramet used a process called chemical vapor deposition (CVD). CVD involves heating precursors for metals, like iridium and rhenium, to temperatures at which they become gaseous. They are then deposited onto a mandrel, or spindle, layer-by-layer to produce high-density, highly resistant materials from the inside out.
Document ID
20020066496
Acquisition Source
Glenn Research Center
Document Type
Other
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Publication Information
Publication: Spinoff 2000
ISBN: 0-16-050462-7
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
ISBN: 0-16-050462-7
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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