NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Fission Reactor Inadvertent Reentry: A Report to the Nuclear Power & Propulsion Technical Discipline TeamThe Nuclear Power and Propulsion Technical Discipline Team has directed an effort to consider possible improvements to the launch approval process as it relates to fission reactors. To that end, Reference 1 described possible general design criteria and risk criteria for fission reactors. At the time that Reference 1 was completed, it was felt that additional examination of reentry issues was warranted. This paper presents the next step in that examination, which is to accurately describe and frame the problem and suggest safety criteria that might apply to inadvertent reentry. The report includes a discussion of the issues associated with different types of inadvertent reentry, the possible consequences of those events, a review of previous work in the area, security and nonproliferation issues, and options for safety requirements that might be considered. Note that safety requirements can have significant mission implications, e.g., no operation below a certain orbit.






Document ID
20190030875
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Camp, Allen
(Consultant Albuquerque, NM)
Borenstein, Elan
(Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
McClure, Patrick
(Los Alamos National Laboratory Los Alamos, NM, United States)
VanDamme, Paul
(Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Voss, Susan
(Global Nuclear Network Analysis, LLC Taos, NM, United States)
Klein, Andy
(Oregon State Univ. Corvallis, OR, United States)
Date Acquired
September 20, 2019
Publication Date
August 1, 2019
Subject Category
Launch Vehicles And Launch Operations
Spacecraft Propulsion And Power
Report/Patent Number
NASA/CR-2019-220397
Funding Number(s)
WBS: 869021.03.07.01.21
CONTRACT_GRANT: 80LARC17C0003
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available