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Subscale Validation of the Subsurface Active Filtration of Exhaust (SAFE) Approach to the NTP Ground TestingNuclear thermal propulsion (NTP) has been recognized as an enabling technology for missions to Mars and beyond. However, one of the key challenges of developing a nuclear thermal rocket is conducting verification and development tests on the ground. A number of ground test options are presented, with the Sub-surface Active Filtration of Exhaust (SAFE) method identified as a preferred path forward for the NTP program. The SAFE concept utilizes the natural soil characteristics present at the Nevada National Security Site to provide a natural filter for nuclear rocket exhaust during ground testing. A validation method of the SAFE concept is presented, utilizing a non-nuclear sub-scale hydrogen/oxygen rocket seeded with detectible radioisotopes. Additionally, some alternative ground test concepts, based upon the SAFE concept, are presented. Finally, an overview of the ongoing discussions of developing a ground test campaign are presented.
Document ID
20150022127
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Marshall, William M.
(NASA Glenn Research Center Cleveland, OH United States)
Borowski, Stanley K.
(NASA Glenn Research Center Cleveland, OH United States)
Bulman, Mel
(Aerojet Rocketdyne, Inc. West Palm Beach, FL, )
Joyner, Russell
(Aerojet Rocketdyne, Inc. West Palm Beach, FL, )
Martin, Charles R.
(National Security Technologies, LLC Las Vegas, NV, United States)
Date Acquired
December 1, 2015
Publication Date
July 27, 2015
Subject Category
Spacecraft Propulsion And Power
Ground Support Systems And Facilities (Space)
Report/Patent Number
GRC-E-DAA-TN24477
Meeting Information
Meeting: Joint Propulsion Conference
Location: Orlando, FL
Country: United States
Start Date: July 27, 2015
End Date: July 29, 2015
Sponsors: Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics, American Society for Engineering Education (ASEE)
Funding Number(s)
WBS: WBS 279585.01.99.99.99.99.22
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Nuclear Rocket Engines
Test facilities (space)
Nuclear Propulsion
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