Calculated Performance of a Direct-Air Nuclear Turbojet-Powered Airplane Using a Split-Flow Reactor and a Separated-Type Shield

Author:	Doyle, R. B.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E50K06
Link:	https://digital.library.unt.edu/ark:/67531/metadc53184/