38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Amp;amp; Exhibit 2002
DOI: 10.2514/6.2002-3678
|View full text |Cite
|
Sign up to set email alerts
|

The Air Force Clustered Hall Thruster Program

Abstract: Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing this collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden to Department of Defense, Washington Headquarters Services, Directorate for Info… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
15
0

Year Published

2002
2002
2023
2023

Publication Types

Select...
5
3

Relationship

3
5

Authors

Journals

citations
Cited by 33 publications
(15 citation statements)
references
References 8 publications
0
15
0
Order By: Relevance
“…6,7 First, the basic operational characteristics of each thruster using a shared cathode depend on whether or not adjacent thrusters are running. This means that there are likely to be cases where a cluster will 4 Walker used the 5-kW P5 thruster, Zakharenkov, et al used a cluster of three 1.5-kW D-55 anode layer thrusters. …”
Section: Discussionmentioning
confidence: 99%
See 2 more Smart Citations
“…6,7 First, the basic operational characteristics of each thruster using a shared cathode depend on whether or not adjacent thrusters are running. This means that there are likely to be cases where a cluster will 4 Walker used the 5-kW P5 thruster, Zakharenkov, et al used a cluster of three 1.5-kW D-55 anode layer thrusters. …”
Section: Discussionmentioning
confidence: 99%
“…First, since thrust was not measured as part of the present investigation, one could hypothesize that the definitive changes in plasma potential, electron temperature, and plasma density profiles discussed above occurred without being accompanied by a change in performance. Second, since both Walker 18 and Zakharenkov, et al, 19 studied larger thrusters, 4 it might be reasonable to suppose that larger thrusters are in some way less sensitive to cathode location than the 200-watt engines studied here. Third, it is possible to hypothesize that there may be a particular design feature (not related to power level) that makes particular thrusters more or less sensitive to cathode position.…”
Section: (5)mentioning
confidence: 99%
See 1 more Smart Citation
“…The Hall thruster is the Busek Company BHT-200-X3 200 W Hall thruster which has been described elsewhere [5]. Table 1 shows the nominal operating conditions for the BHT-200-X3 thruster for this test.…”
Section: Apparatusmentioning
confidence: 99%
“…4 A cluster of thrusters may have a slightly lower efficiency and higher dry mass than a similarly powered monolithic thruster since larger thrusters have historically performed better than smaller thrusters. However, the clustered approach does have several advantages, including improved system reliability due to the inherent redundancy of running multiple engines, as well as the ability to throttle the system by simply turning off one or more of the thrusters.…”
Section: Introductionmentioning
confidence: 99%