NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
NPSP selection for a nuclear rocket.Twin spool zero-NPSP /net positive suction pressure/ turbopump selected for NERVA rocket after assessing turbopump, engine, vehicle and mission related systems
Document ID
19670055217
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Beveridge, J. H.
Campbell, W. E.
Fitts, J. J.
Date Acquired
August 3, 2013
Publication Date
July 1, 1967
Subject Category
Nuclear Engineering
Report/Patent Number
AIAA PAPER 67-476
Report Number: AIAA PAPER 67-476
Accession Number
67A33946
Distribution Limits
Public
Copyright
Other
Keywords
TURBOPUMP
ROCKET ENGINE
SYSTEM FAILURE
NUCLEAR ENGINE FOR ROCKET VEHICLE /NERVA/

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available