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Overview of the Main Propulsion System for a Nuclear Thermal Propulsion Flight DemonstratorA demonstration of a Nuclear Thermal Propulsion (NTP) engine has not been conducted in over 50 years. Several tests were conducted during the NERVA program but no NTP engine was ever flown in space. In the last several years there has been a considerable amount of conceptual design work on NTP engines conducted. With the prospect of human Mars missions in the 2030’s there has been a renewed interest in NTP engines. A concept design study was conducted with the intent to design 2 flight demonstrator vehicles that would buy down programmatic and technical risks associated with launching and operating nuclear reactors in space. The intent of the first demonstrator mission would be to employ a simplified NTP engine and buy down programmatic risks whereas the second demonstrator would buy down technical risks with a NTP engine designed to be similar to an operational NTP model. The results of the study showed that a simplified NTP engine demonstrator could be feasibly built and flown in the near term with mostly high TRL, commercial off-the-shelf components.
Document ID
20200001000
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Simpson, S. P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bean, Q. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rodriguez, M. A.
(Jacobs Engineering Group Huntsville, AL, United States)
Date Acquired
February 20, 2020
Publication Date
December 9, 2019
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M19-7762
Meeting Information
Meeting: Liquid Propulsion (LPS)
Location: Tampa, FL
Country: United States
Start Date: December 9, 2019
End Date: December 13, 2019
Sponsors: Department of the Navy, NASA Headquarters, Department of the Air Force, Department of the Army
Distribution Limits
Public
Copyright
Public Use Permitted.
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