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학술연구

HTPB 기반 고체 추진제의 열팽창계수 특성에 관한 실험적 연구 : 배치 간 변동성 및 가속 노화 영향 분석

원문정보

Experimental Study on Thermal Expansion Coefficient Characteristics of HTPB-based Solid Propellant : Analysis of Batch-to-Batch Variability and Accelerated Aging Effects

오대산, 박순우, 정민주, 김영현

피인용수 : 0(자료제공 : 네이버학술정보)

초록

영어

This study investigates the thermal expansion characteristics of hydroxyl-terminated polybutadiene(HTPB) based solid propellants, focusing on batch-to-batch variability and accelerated aging effects. Coefficient of thermal expansion(CTE) measurements were conducted using thermomechanical analyzer(TMA) on samples from different manufacturing batches and specimens aged at various temperatures for different durations. Results indicate variations in CTE values between batches, highlighting the significance of manufacturing process control. Accelerated aging experiments reveal minimal systematic changes in CTE, suggesting stability of thermal expansion properties under short-term thermal stress. The overall distribution of CTE values shows concentration within a specific range, indicating consistency in thermal expansion characteristics. These findings provide insights into the thermal behavior of HTPB-based solid propellants, contributing to improved missile design and lifecycle prediction models.

목차

Abstract
1. 서론
2. 실험방법
3. 결과 및 고찰
4. 결론
References

저자정보

  • 오대산 Dae-San Oh. Member, Defense Agency for Technology and Quality
  • 박순우 Soon-Woo Park. Member, Defense Agency for Technology and Quality
  • 정민주 Min-Ju Jeong. Member, Defense Agency for Technology and Quality
  • 김영현 Yeong-Hyeon Kim. Member, Defense Agency for Technology and Quality

참고문헌

자료제공 : 네이버학술정보

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