SYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM

SYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM

The fighter aircraft development project is the first experience for PT Dirgantara Indonesia (Persero). The system safety analysis process that refers to military standards is needed in the development of fighter aircraft. The purpose of this research was to develop a system safety assessment pro...

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Main Author: Iman Effendi, Nurul
Format: Theses
Language:Indonesia
Subjects:
Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
Online Access:https://digilib.itb.ac.id/gdl/view/37887
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:37887
spelling id-itb.:378872019-04-25T14:46:54ZSYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM Iman Effendi, Nurul Teknik (Rekayasa, enjinering dan kegiatan berkaitan) Indonesia Theses System safety assessment, system safety analysis, MIL-STD-882E, JSSG 2001B, hazard analysis, preliminary hazard analysis, subsystem hazard analysis, system hazard analysis, air vehicle noncombat loss rate, PT Dirgantara Indonesia. INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/37887 The fighter aircraft development project is the first experience for PT Dirgantara Indonesia (Persero). The system safety analysis process that refers to military standards is needed in the development of fighter aircraft. The purpose of this research was to develop a system safety assessment procedure based on MILSTD- 882E and JSSG 2001B, conduct a system safety assessment and conduct a system safety assessment analysis. This research applies system safety analysis to T-103X aircraft flight control system based on MIL-STD-882E. System safety assessment is implemented by conducting preliminary hazards analysis, subsystems hazards analysis, system hazards analysis and software functional hazard analysis. All identified hazards are given recommendations actions to reduce the risk of failure to an acceptable level. The results of the air vehicle noncombat loss rate comply to the requirements acchieve 4.38 x 10-12 flight hours. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
topic Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
spellingShingle Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
Iman Effendi, Nurul
SYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM
description The fighter aircraft development project is the first experience for PT Dirgantara Indonesia (Persero). The system safety analysis process that refers to military standards is needed in the development of fighter aircraft. The purpose of this research was to develop a system safety assessment procedure based on MILSTD- 882E and JSSG 2001B, conduct a system safety assessment and conduct a system safety assessment analysis. This research applies system safety analysis to T-103X aircraft flight control system based on MIL-STD-882E. System safety assessment is implemented by conducting preliminary hazards analysis, subsystems hazards analysis, system hazards analysis and software functional hazard analysis. All identified hazards are given recommendations actions to reduce the risk of failure to an acceptable level. The results of the air vehicle noncombat loss rate comply to the requirements acchieve 4.38 x 10-12 flight hours.
format Theses
author Iman Effendi, Nurul
author_facet Iman Effendi, Nurul
author_sort Iman Effendi, Nurul
title SYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM
title_short SYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM
title_full SYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM
title_fullStr SYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM
title_full_unstemmed SYSTEM SAFETY ASSESSMENT FOR T-103X FLIGHT CONTROL SYSTEM
title_sort system safety assessment for t-103x flight control system
url https://digilib.itb.ac.id/gdl/view/37887
_version_ 1822924924052832256

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