NTRS
NTRS - NASA Technical Reports Server
Search
more_vert
Collections
About
News
Help
Login
Press Enter or click the Search button to begin your search.
Back to Results
OUTLOOK FOR GAS-CORE NUCLEAR ROCKETS
Fission energy transferal, hydrogen propellant flow, and adequate fissionable material are main factors in gas-core nuclear rocket design concepts
Document ID
19630024215
Acquisition Source
Legacy CDMS
Document Type
Abstract
Authors
Ragsdale, R. G.
Date Acquired
August 1, 2013
Publication Date
August 1, 1963
Subject Category
Propellants
Accession Number
63A20274
Distribution Limits
Public
Copyright
Other
Keywords
GASEOUS FISSION REACTOR
ROCKET ENGINE
REACTOR
Available Downloads
There are no available downloads for this record.
Related Records
There are no records associated with this record.
visibility_off
No Preview Available