DocumentCode
2789448
Title
Design and implementation of KSLV-I telemetry system with MIL-STD-1553B
Author
Kim, Joonyun ; Jung, Haeseung ; Kim, Bo-Gwan
Author_Institution
Dept. of Electron., Korea Aerosp. Res. Inst., Daejon
fYear
2005
fDate
5-12 March 2005
Firstpage
1292
Lastpage
1299
Abstract
KSLV (Korea Space Launch Vehicle)-I is under development to place a 100-kg class satellite into a low earth orbit of 300times1500km. KSLV-I telemetry system will be composed of two telemetry streams: a lower (first) stage telemetry stream and an upper (second) stage telemetry stream. Different from the previously developed telemetry system by KARI for KSR (Korea Sounding Rocket) series, the new telemetry system has been required to meet the enhanced requirements on telemetry system. This paper introduces a new development of telemetry system for KSLV-I upper stage telemetry with MIL-STD-1553B data bus emphasizing on the design, implementation, evaluation test and salient features of the telemetry system
Keywords
rockets; satellite telemetry; KSLV-I telemetry system; Korea space launch vehicle; MIL-STD-1553B; data bus; telemetry streams; Aerospace electronics; Aerospace engineering; Data acquisition; Electric shock; Low earth orbit satellites; Payloads; Phase change materials; Prototypes; System testing; Telemetry;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2005 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-8870-4
Type
conf
DOI
10.1109/AERO.2005.1559419
Filename
1559419
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