NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Magnetohydrodynamic Augmented Propulsion ExperimentOver the past several years, efforts have been under way to design and develop an operationally flexible research facility for investigating the use of cross-field MHD accelerators as a potential thrust augmentation device for thermal propulsion systems. The baseline configuration for this high-power experimental facility utilizes a 1.5-MWe multi-gas arc-heater as a thermal driver for a 2-MWe MHD accelerator, which resides in a large-bore 2-tesla electromagnet. A preliminary design study using NaK seeded nitrogen as the working fluid led to an externally diagonalized segmented MHD channel configuration based on an expendable heat-sink design concept. The current status report includes a review of engineering/design work and performance optimization analyses and summarizes component hardware fabrication and development efforts, preliminary testing results, and recent progress toward full-up assembly and testing
Document ID
20080033025
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Litchford, Ron J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
May 30, 2008
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 2008 Annual Technical Meeting
Location: Yamanakako
Country: Japan
Start Date: May 30, 2008
End Date: May 31, 2008
Sponsors: Japan MHD Society
Funding Number(s)
CONTRACT_GRANT: SAA8-05786
CONTRACT_GRANT: SAA8-05952
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available