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An End-To-End Test of A Simulated Nuclear Electric Propulsion SystemThe Safe Affordable Fission Engine (SAFE) test series addresses Phase I Space Fission Systems issues in it particular non-nuclear testing and system integration issues leading to the testing and non-nuclear demonstration of a 400-kW fully integrated flight unit. The first part of the SAFE 30 test series demonstrated operation of the simulated nuclear core and heat pipe system. Experimental data acquired in a number of different test scenarios will validate existing computational models, demonstrated system flexibility (fast start-ups, multiple start-ups/shut downs), simulate predictable failure modes and operating environments. The objective of the second part is to demonstrate an integrated propulsion system consisting of a core, conversion system and a thruster where the system converts thermal heat into jet power. This end-to-end system demonstration sets a precedent for ground testing of nuclear electric propulsion systems. The paper describes the SAFE 30 end-to-end system demonstration and its subsystems.
Document ID
20020087938
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
VanDyke, Melissa
(NASA Marshall Space Flight Center Huntsville, AL United States)
Hrbud, Ivana
(Engineering Research and Consulting, Inc. Huntsville, AL United States)
Goddfellow, Keith
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Rodgers, Stephen L.
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: 38th AIAA Joint Propulsion Conference
Location: Indianapolis, IN
Country: United States
Start Date: July 7, 2002
End Date: July 10, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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