Failure mode effect analysis for a better functional composite rocket motor casing

Srivastava, Lokesh; Lanka, Krishnanand; Behera, Sameerkant; Nath, N. Kishore

doi:10.1016/j.matpr.2022.04.933

Cited by 4 publications

(2 citation statements)

References 12 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Risk assessment for solid-propellant rocket motor has conducted by several researcher. Srivastava et al, [1] studied composite rocket motor casing using Failure Mode Effect Analysis (FMEA) and Failure Mode Effect and Criticality Analysis (FMECA) methods. They performed qualitative analysis in line with MIL-STD-1629A and quantitative analysis using FMECA Risk Priority Number (RPN).…”

Section: Introductionmentioning

confidence: 99%

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

Deswandri,

Ratih Luhuring Tyas,

Dinnia Intaningrum

et al. 2023

ARFMTS

View full text Add to dashboard Cite

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.

show abstract

Section: Introductionmentioning

confidence: 99%

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

Deswandri,

Ratih Luhuring Tyas,

Dinnia Intaningrum

et al. 2023

ARFMTS

View full text Add to dashboard Cite

show abstract

“…Owing to the manufacturing process, CRMCs are often designed for refinement with possible failures in the dome or some critical areas (Özaslan et al, 2022;Srivastava et al, 2022a;Wu et al, 2022). This is highly detrimental to the overall safety of the SRM.…”

Section: Introductionmentioning

confidence: 99%

Multiscale analyses of the damage of composite rocket motor cases

Zai

Hui²,

Cao

2023

Front. Mater.

View full text Add to dashboard Cite

As one of the key components of solid rocket motors (SRMs) and launch vehicles (LVs), the deformation and damage of the composite rocket motor case (CRMC) can directly affect the effectiveness of the SRMs. Therefore, it is particularly important to analyze the damage failure of composite cases. As the analysis remains complex due to the different failure modes of composites at different scales, this paper applies multiscale analysis methods to CRMC damage. A multiscale mechanical model of CRMC is established, and data transfer between the microscale, mesoscale, and macroscale models is achieved using submodel techniques. In this paper, CRMC was finely modeled, and the thickness and carbon fiber angle of each fiber winding layer were accurately described. Additionally, the results of hydrostatic tests and numerical calculations were compared to verify the validity of the modeling method. The stress levels of the material at macroscale, mesoscale, and microscale scales were obtained through numerical calculations, and the microscale damage failure behavior of the material under the internal pressure load of the composite shell was predicted by combining the strength assessment criterion.

show abstract

Mapping quality assurance using a HAZOP study by performing failure detection method on solid rocket motor casing

Junianto,

Meliana,

Abrizal

et al. 2024

5TH INTERNATIONAL SEMINAR ON METALLURGY AND MATERIALS (ISMM2022): Strengthening Research and Innovation in Metallurgy and Mater

View full text Add to dashboard Cite

Failure mode effect analysis for a better functional composite rocket motor casing

Cited by 4 publications

References 12 publications

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

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

Multiscale analyses of the damage of composite rocket motor cases

Mapping quality assurance using a HAZOP study by performing failure detection method on solid rocket motor casing

Contact Info

Product

Resources

About