30 cm Engineering Model thruster design and qualification tests

Schnelker, D. E.; Collett, C. R.

doi:10.2514/6.1975-341

Search citation statements

Order By: Relevance

Paper Sections

Select...

Grid Geometry Variation1

Original Page Is Of Poor Quality1

Citation Types

Supporting

Mentioning

Contrasting

Year Published

1976

Publication Types

Select...

Other3

Relationship

Self Cite0

Independent3

Authors

Journals

Cited by 3 publications

(2 citation statements)

References 0 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…To illustrate this method, the 30-cm diameter Engineering Model electron-bombardment ion thruster, currently being developed as a primary propulsion source for extended space missions [15], is analyzed to predict its ion-optical performance. The non-dimensionalized grid set parameters for this thruster are as follows: Step I.…”

Section: Grid Geometry Variationmentioning

confidence: 99%

The ion optics of a two grid electron-bombardment thruster

Aston

Kaufman

1976

12th International Electric Propulsion Conference

View full text Add to dashboard Cite

Section: Grid Geometry Variationmentioning

confidence: 99%

The ion optics of a two grid electron-bombardment thruster

Aston

Kaufman

1976

12th International Electric Propulsion Conference

View full text Add to dashboard Cite

“…16 The present 900 aeries ehrusters^` incorporate modifications of the internal thruster components to minimize sputtering-spalling effects. These include cladding the deposition sites such an the anode and backplate with grit blasted wire mesh, cladding the bufflu, baffle mount and cathode pole piece with rental= and reverting back to the sue of the modified 400 aeries baffle mount.…”

Section: Original Page Is Of Poor Qualitymentioning

confidence: 99%