10th Electric Propulsion Conference 1973
DOI: 10.2514/6.1973-1138
|View full text |Cite
|
Sign up to set email alerts
|

Investigation of hollow cathode performance for 30-cm thrusters

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

1973
1973
1981
1981

Publication Types

Select...
4
1
1

Relationship

0
6

Authors

Journals

citations
Cited by 13 publications
(1 citation statement)
references
References 3 publications
0
1
0
Order By: Relevance
“…Cathode erosion raves may be adequately correlated with discharge current level and cathode orifice diameter. (10,12) It was desired to obtain a cathode that exhibited the following: case of starting, low thermal loading due to die.. charge self heating, stability during a high voltage 4ecycle and an acceptable V-I characteristic for discharge currents from 10 to 25 A. Figure 8 illustrates the variation of discharge voltage with discharge chamber magnetic field strength for cathodes with orifice diameters' of 0.75 and 1.52 mm.…”
Section: Discharge Chamber Cathode Performancementioning
confidence: 99%
“…Cathode erosion raves may be adequately correlated with discharge current level and cathode orifice diameter. (10,12) It was desired to obtain a cathode that exhibited the following: case of starting, low thermal loading due to die.. charge self heating, stability during a high voltage 4ecycle and an acceptable V-I characteristic for discharge currents from 10 to 25 A. Figure 8 illustrates the variation of discharge voltage with discharge chamber magnetic field strength for cathodes with orifice diameters' of 0.75 and 1.52 mm.…”
Section: Discharge Chamber Cathode Performancementioning
confidence: 99%