Recent progress in high specific impulse thermo-ionic acceleration.Thermionic cathode jet accelerator performance data and comparison between hydrogen and deuterium propellant use
Document ID
19650033883
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ducati, A. C.
Giannini, G. M.
Muehlberger, E.
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 65-96Report Number: AIAA PAPER 65-96
Accession Number
65A16587
Funding Number(s)
CONTRACT_GRANT: AF 49/638/-1161 CONTRACT_GRANT: NASW-968