2016
DOI: 10.1061/(asce)as.1943-5525.0000638
|View full text |Cite
|
Sign up to set email alerts
|

Optimal Station Keeping for XIPS Thrusters in Failure Mode under Eclipse Constraints

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2017
2017
2024
2024

Publication Types

Select...
5

Relationship

0
5

Authors

Journals

citations
Cited by 6 publications
(1 citation statement)
references
References 23 publications
0
1
0
Order By: Relevance
“…geosynchronous Earth-orbit communication satellite upkeep (XIPS thruster [3], …) to asteroid probing (Deep Space 1 [4], Dawn [5], Hayabusa/Hayabusa 2 [6], …). Current state-of-the-art concerns application of the 6.9 kW NEXT-C in NASA's double asteroid redirection test through spacecraft impact-induced deflection of the minor-planet moon Dimorphos [7].…”
Section: Introductionmentioning
confidence: 99%
“…geosynchronous Earth-orbit communication satellite upkeep (XIPS thruster [3], …) to asteroid probing (Deep Space 1 [4], Dawn [5], Hayabusa/Hayabusa 2 [6], …). Current state-of-the-art concerns application of the 6.9 kW NEXT-C in NASA's double asteroid redirection test through spacecraft impact-induced deflection of the minor-planet moon Dimorphos [7].…”
Section: Introductionmentioning
confidence: 99%