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Metallic Hydrogen - Potentially a High Energy Rocket PropellantPure metallic hydrogen is predicted to have a specific impulse (Isp) of 1700 seconds, but the reaction temperature is too high for current engine materials. Diluting metallic hydrogen with liquid hydrogen can reduce the reaction temperature to levels compatible with current material limits and still provide an Isp greater than 900 s. Metallic hydrogen has not yet been produced on earth, but experimental techniques exist that may change this situation. This paper will provide a brief description of metallic hydrogen and the status of experiments that may soon produce detectable quantities of this material in the lab. Also provided are some characteristics for diluted metallic hydrogen engines and launch vehicles.
Document ID
20080018926
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Cole, John
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Silvera, Ike
(Harvard Univ. Cambridge, MA, United States)
Date Acquired
August 24, 2013
Publication Date
October 26, 2007
Subject Category
Propellants And Fuels
Meeting Information
Meeting: Tennessee Valley Emerging Technology Conference
Location: Huntsville, AL
Country: United States
Start Date: March 26, 2008
End Date: March 28, 2008
Sponsors: Defense Intelligence Agency, Army Strategic Defense Command
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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