RIT15S and RIT 15 LP - The development of high performance mission optimized ion thrusters-Reference-Cited by-同舟云学术

RIT15S and RIT 15 LP - The development of high performance mission optimized ion thrusters

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Leiter H.¹,Loeb H.¹,Schartner K.-H.¹

Affiliation:

1. Giessen, Univ., Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2444

Reference12 articles.

1. [l] K.H. Groh,H.J.Leiter,H.W. Lob RIT 15:A mediumthrustrangeradiofrequencyion thrusterProceedingsof theSecondEuropean SpacecraftPropulsionConference,P203 ESTEC,Nordwijk 1997,page377-382

2. H.Bassner,R.A Bond,V.K. ThompsonK.Groh TheESA-XX ionthruster Proceedingsof theSecondEuropeanSpacecraft PropulsionConference,page25l-257 ESTEC,Nordwijk 1997

3. JuergenMueller, JohnR.Brophy,D. Kyle Brown Design,FabricationandTestingof 30cmDia.Dished Carbon-CarbonIonEngineGrids AIAA Paper96-3204,LakeBueneVista 1996

4. [S]J.S.Meserole,M.E. Rorabough FabricationandTestingof 15cmCarbon-Carbon Gridswith Slit Apertures AIAA Paper95-2661,SanDiego 1995

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