Ground Firing Tests of Standard Motor and System Sizing for Long Duration Divert and Attitude Control System

This paper describes the results of standard motor tests by propellant formulation conducted for the development of long-duration DACS (Divert and Attitude Control System) and the system sizing derived from these results.Standard motor testing confirmed that stable combustion without the use of metallic stabilizers, and a burn rate correction factor was derived and applied to system sizing.The system sizing analysis indicates that propellant E is suitable for DCS (Divert Control System) and propellant A for ACS (Attitude Control System); the final selection, however, will be confirmed after additional evaluation of material compatibility. (DACS) . , . , (DCS) propellant E, (ACS) propellant A , DACS .

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Publication Details

Journal
Journal of the Korean Society of Propulsion Engineers
Published
2026-04-30
DOI
https://doi.org/10.6108/kspe.2026.30.2.031
Primary Topic
Spacecraft and Cryogenic Technologies
Type
article
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article

Ground Firing Tests of Standard Motor and System Sizing for Long Duration Divert and Attitude Control System

Jisu Yoon, Byungsun Min, Junyoung Heo, Dongsung Ha et al.
Journal of the Korean Society of Propulsion Engineers
Spacecraft and Cryogenic Technologies
article

Ground Firing Tests of Standard Motor and System Sizing for Long Duration Divert and Attitude Control System

Jisu Yoon, Byungsun Min, Junyoung Heo, Dongsung Ha, Seongjoo Han
article en

Abstract

This paper describes the results of standard motor tests by propellant formulation conducted for the development of long-duration DACS (Divert and Attitude Control System) and the system sizing derived from these results.Standard motor testing confirmed that stable combustion without the use of metallic stabilizers, and a burn rate correction factor was derived and applied to system sizing.The system sizing analysis indicates that propellant E is suitable for DCS (Divert Control System) and propellant A for ACS (Attitude Control System); the final selection, however, will be confirmed after additional evaluation of material compatibility. (DACS) . , . , (DCS) propellant E, (ACS) propellant A , DACS .

Journal of the Korean Society of Propulsion EngineersVol. 30(2)
Agency for Defense Development (KR)
Affordable and clean energy
Openalex Percentile: Top 1%
Spacecraft and Cryogenic Technologies
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Ground Firing Tests of Standard Motor and System Sizing for Long Duration Divert and Attitude Control System — Jisu Yoon, Byungsun Min, et al. · Journal of the Korean Society of Propulsion Engineers (2026) | TGRS Research Map | TGRS