Risk Assessment of Solid Propellant Rocket Motor using a Combination of HAZOP and FMEA Methods

Authors

  • Deswandri Research Center for Nuclear Reactor Technology, Research Organization for Nuclear Energy, National Research and Innovation Agency (BRIN), Kawasan Puspiptek Gd. 80, Tangerang Selatan, 15314, Banten, Indonesia
  • Ratih Luhuring Tyas Research Center for Nuclear Reactor Technology, Research Organization for Nuclear Energy, National Research and Innovation Agency (BRIN), Kawasan Puspiptek Gd. 80, Tangerang Selatan, 15314, Banten, Indonesia
  • Dinnia Intaningrum Research Center for Safety, Metrology and Nuclear Quality Technology, Research Organization for Nuclear Energy, National Research and Innovation Agency (BRIN), Kawasan Puspiptek Gd. 71, Tangerang Selatan, 15314, Banten, Indonesia
  • Idris Eko Putro Research Center for Rocket Technology, Research Organization for Aeronautics and Space, National Research and Innovation Agency (BRIN), Jalan Raya Lapan, Mekar Sari, Bogor Parungpanjang, Kabupaten Bogor, 16350, Jawa Barat, Indonesia
  • Ahmad Riyadl Research Center for Rocket Technology, Research Organization for Aeronautics and Space, National Research and Innovation Agency (BRIN), Jalan Raya Lapan, Mekar Sari, Bogor Parungpanjang, Kabupaten Bogor, 16350, Jawa Barat, Indonesia
  • Irvan Dwi Junianto Research Center for Safety, Metrology and Nuclear Quality Technology, Research Organization for Nuclear Energy, National Research and Innovation Agency (BRIN), Kawasan Puspiptek Gd. 71, Tangerang Selatan, 15314, Banten, Indonesia
  • Alfitri Meliana Directorate of Laboratory Management, Research Facilities, and Science and Technology Park, Deputy for Research and Innovation Infrastructure, National Research and Innovation Agency (BRIN), Kawasan Puspiptek, Tangerang Selatan, 15314, Banten, Indonesia
  • Rika Andiarti Research Center for Rocket Technology, Research Organization for Aeronautics and Space, National Research and Innovation Agency (BRIN), Jalan Raya Lapan, Mekar Sari, Bogor Parungpanjang, Kabupaten Bogor, 16350, Jawa Barat, Indonesia
  • Arif Nur Hakim Research Center for Rocket Technology, Research Organization for Aeronautics and Space, National Research and Innovation Agency (BRIN), Jalan Raya Lapan, Mekar Sari, Bogor Parungpanjang, Kabupaten Bogor, 16350, Jawa Barat, Indonesia

DOI:

https://doi.org/10.37934/arfmts.110.1.6378

Keywords:

Solid-propellant Rocket Motor (SRM), Risk assessment, HAZOP, FMEA

Abstract

The development of rockets in Indonesia has long been carried out by the National Aeronautics and Space Agency (LAPAN), which has now been integrated into the National Research and Innovation Agency (BRIN). The Research Centre for Rocket Technology, which is one of the centres within BRIN, has been developing solid propellant-based rockets with a various sizes and types. Solid-propellant rocket technology is commonly used because of their reliability, cost-effectiveness, and simple design. However, this technology is one of the high-risk technologies, whose failure can harm humans, damage the environment and cause huge losses to assets. As a high-risk technology, risk assessment activities must be carried out, starting from the design, manufacturing, testing and up to the launching stage. In this paper, we studied a risk assessment for general Solid-propellant Rocket Motor (SRM). SRM is basically a device that processes chemical energy in solid propellant into thrust (kinetic energy) in a container that functions as a pressure vessel. The risk assessment methods commonly used in this technology are the HAZOP or FMEA methods. The HAZOP is excellent in identifying failure modes systematically through identifying the deviation of physical process parameters but has difficulties in prioritizing the risk. The FMEA has effectiveness in understanding failure mechanisms and establishing necessary countermeasures, but for a product with a lot of components, the worksheet is also complex. By combining these two methods, integrating the superiority of each method, this research can identify modes, causes and effects of failure that may occur in SRM effective and accurately. In addition, this research also proposes corrective or preventive actions for each failure mode. As the objective of the risk assessment, results of the research can be used as input for the designers to improve their design and as inspection and surveillance objects for QC officers.

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Author Biographies

Deswandri, Research Center for Nuclear Reactor Technology, Research Organization for Nuclear Energy, National Research and Innovation Agency (BRIN), Kawasan Puspiptek Gd. 80, Tangerang Selatan, 15314, Banten, Indonesia

desw002@brin.go.id

Ratih Luhuring Tyas, Research Center for Nuclear Reactor Technology, Research Organization for Nuclear Energy, National Research and Innovation Agency (BRIN), Kawasan Puspiptek Gd. 80, Tangerang Selatan, 15314, Banten, Indonesia

rati009@brin.go.id

Dinnia Intaningrum, Research Center for Safety, Metrology and Nuclear Quality Technology, Research Organization for Nuclear Energy, National Research and Innovation Agency (BRIN), Kawasan Puspiptek Gd. 71, Tangerang Selatan, 15314, Banten, Indonesia

dinn002@brin.go.id

Idris Eko Putro, Research Center for Rocket Technology, Research Organization for Aeronautics and Space, National Research and Innovation Agency (BRIN), Jalan Raya Lapan, Mekar Sari, Bogor Parungpanjang, Kabupaten Bogor, 16350, Jawa Barat, Indonesia

idri001@brin.go.id

Ahmad Riyadl, Research Center for Rocket Technology, Research Organization for Aeronautics and Space, National Research and Innovation Agency (BRIN), Jalan Raya Lapan, Mekar Sari, Bogor Parungpanjang, Kabupaten Bogor, 16350, Jawa Barat, Indonesia

ahma052@brin.go.id

Irvan Dwi Junianto, Research Center for Safety, Metrology and Nuclear Quality Technology, Research Organization for Nuclear Energy, National Research and Innovation Agency (BRIN), Kawasan Puspiptek Gd. 71, Tangerang Selatan, 15314, Banten, Indonesia

irva006@brin.go.id

Alfitri Meliana, Directorate of Laboratory Management, Research Facilities, and Science and Technology Park, Deputy for Research and Innovation Infrastructure, National Research and Innovation Agency (BRIN), Kawasan Puspiptek, Tangerang Selatan, 15314, Banten, Indonesia

alfi008@brin.go.id

Rika Andiarti, Research Center for Rocket Technology, Research Organization for Aeronautics and Space, National Research and Innovation Agency (BRIN), Jalan Raya Lapan, Mekar Sari, Bogor Parungpanjang, Kabupaten Bogor, 16350, Jawa Barat, Indonesia

rika001@brin.go.id

Arif Nur Hakim, Research Center for Rocket Technology, Research Organization for Aeronautics and Space, National Research and Innovation Agency (BRIN), Jalan Raya Lapan, Mekar Sari, Bogor Parungpanjang, Kabupaten Bogor, 16350, Jawa Barat, Indonesia

arif014@brin.go.id

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Published

2023-12-03

How to Cite

Deswandri, Ratih Luhuring Tyas, Dinnia Intaningrum, Idris Eko Putro, Ahmad Riyadl, Irvan Dwi Junianto, Alfitri Meliana, Rika Andiarti, & Arif Nur Hakim. (2023). Risk Assessment of Solid Propellant Rocket Motor using a Combination of HAZOP and FMEA Methods. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 110(1), 63–78. https://doi.org/10.37934/arfmts.110.1.6378

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