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
Transient and Steady Performance of an Ion Rocket Thrust Augmentor Final ReportPerformance of ion rocket thrust augmentor, Langmuir probe measurements, secondary electron emission from porous tungsten, and heat transfer from large diameter Pirani pressure gauges
Document ID
19660027496
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
CER66-67VAS3
NASA-CR-77855
Report Number: CER66-67VAS3
Report Number: NASA-CR-77855
Accession Number
66N36786
Funding Number(s)
CONTRACT_GRANT: NSG-570
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
IONIC PROPULSION
PIRANI GAUGE
ELECTRON EMISSION
HEAT TRANSFER
LANGMUIR PROBE

Related Records

IDRelationTitle19660027497WorkOperation of one-half inch diameter ion thrustor with a countercurrent electron accelerator19660027498WorkLangmuir probe measurements19660027499WorkSecondary electron emission19660027500WorkHeat transfer from large diameter Pirani gauges operating down to a microtorr19660027497WorkOperation of one-half inch diameter ion thrustor with a countercurrent electron accelerator19660027498WorkLangmuir probe measurements19660027499WorkSecondary electron emission19660027500WorkHeat transfer from large diameter Pirani gauges operating down to a microtorr
No Preview Available