메뉴 건너뛰기
Library Notice
Institutional Access
If you certify, you can access the articles for free.
Check out your institutions.
ex)Hankuk University, Nuri Motors
Log in Register Help KOR
Subject
Humanities
General Humanities History Philosophy Religious Studies Linguistics and Literature Other Humanities
Social science
General Social Science Business Management Tourism Education Military Science Library and Information Science Law Sociology Journalism and Media Studies Psychological Science Political Science and Diplomacy Geography Public Administration Economics International Trade Anthropology Other Social Science
Natural science
General Natural Science Physics Biology Life Sciences Mathematics/Statistics Astronomy Earth Science Chemistry Other Natural Science
Engineering
General Engineering Architectural Engineering Mechanical Engineering Industrial Engineering Material/Energy Engineering Electrical and Electronic Engineering Marine and Ocean Engineering Chemical Engineering Computer Science Other Engineering
Medical science
General Medical Science Nursing Science Veterinary Pharmacy Traditional Korean Medicine Basic Medicine Clinical Medicine Other Medicine
Agriculture and Fishery
General Agriculture and Fishery Agriculture Fishery Science Food Science Forestry Animal Husbandry Marine Transportation Studies Other Agriculture and Fishery
Art and Kinesiology
General Arts Design Fine Arts Cosmetology Photography Music Fashion Kinesiology Performing Media Arts Other Arts and Kinesiology
Interdisciplinary Studies
Interdisciplinary Research Science and Technology Studies Brain and Cognitive Science Technology Policy Other Interdisciplinary Studies

KOR

Ignition Characteristic of Low-toxic Hypergolic Propellant According to Fuel Properties
Recommendations
Search
Questions

연료 물성에 따른 저독성 접촉점화 추진제의 점화 특성

논문 기본 정보

Type
Academic journal
Author
Chungman Kim (Hanbat National University) Hongjae Kang (Korea Institute of Machinery and Materials) Kyounghwan Lee (Korea Research Institute for defense Technology planning and advancement) Jongkwang Lee (Hanbat National University)
Journal
The Korean Society for Aeronautical & Space Sciences Journal of the Korean Society for Aeronautical & Space Sciences Vol.52 No.2 KCI Excellent Accredited Journal SCOPUS
Published
2024.2
Pages
131 - 137 (7page)
DOI
10.5139/JKSAS.2024.52.2.131

Usage

cover
📌
Topic
📖
Background
🔬
Method
🏆
Result
Ignition Characteristic of Low-toxic Hypergolic Propellant According to Fuel Properties
Ask AI
Recommendations
Search
Questions

Research history (4)

2024

Ignition Characteristic of Low-toxic Hypergolic Propellant According to Fuel Properties
Chungman Kim ,  Hongjae Kang ,  Kyounghwan Lee and others 1 Journal of the Korean Society for Aeronautical & Space Sciences 2024.02 Academic journal

2023

Ignition characteristics for hypergolic propellant base on H₂O₂ using doublet injector
Chungman Kim ,  Byungwoo Choi ,  Hongjae Kang and others 1 한국추진공학회 학술대회논문집 2023.11 Proceeding
Research and Review of Impinging Jet Test for Low-toxicity Hypergolic Propellant
Chungman Kim ,  Hongjae Kang ,  Kyounghwan Lee and others 1 Journal of the Korean Society of Propulsion Engineers 2023.06 Academic journal
Impinging Jet Test Device Manufacture of Hypergolic Propellant
Chungman Kim ,  Hongjae Kang ,  Kyounghwan Lee and others 1 한국추진공학회 학술대회논문집 2023.05 Proceeding
  • Are you curious about the follow-up research of this article?
  • You can check more advanced research results through related academic papers or academic presentations.
  • Check the research history of this article

Abstract· Keywords

Report Errors
The ignition performance of hypergolic propellant is judged by ignition delay. Ignition performance could be evaluated through a drop test and a impinging jet test. The impinging get test is a method that induces a rapid chemical reaction through mixing and atomization of propellant by impinging propellant column. Physical properties of propellant affect the propellant column injected into the injector, so that the ignition performance could be changed by physical properties of propellant. In this paper, We were performed a drop test and a impinging jet test by using fuel with large differenced viscosity and vapor pressure. High-viscosity fuel had improved ignition performance with momentum, while Low-viscosity fuel with high vapor pressure had sporadic ignition phenomena and short ignition delay regardless of the momentum.
#Impinging Jet Test(액주 충돌 실험) #Drop Test(액적 낙하 실험) #Hypergolic Propellant(접촉점화 추진제) #Hydrogen Peroxide(과산화수소)

Contents

ABSTRACT
초록
Ⅰ. 서론
Ⅱ. 본론
Ⅲ. 결론
References

References (7)

Add References
Kim, S. K., Chae, J. W., Won, S. H. and Jun, H. Y., “Status and Prospect of Spacecraft Propulsion system,” Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 44, No. 8, 2016, pp. 695~701. google schola Park, S. H., Kang, H. J., Park, Y. C. and Lee, J. K., “A Review of the Technical Development on Green Hypergolic Propellant,” Journal of the Korean Society of Propulsion Engineers, Vol. 24, No. 4, 2020, pp. 79~88. google schola Florczuk, W. and Rarate, G., “Assessment of various fuel additives for reliable hypergolic ignition with 98% HTP,” 66 th International Astronautical Congress, October 2015, IAC-15-C4.3.9. google schola Kim, C. M., Kang, H. J., Lee, K. H. and Lee, J. K., “Research and Review of Impinging Jet Test for Low-toxicity Hypergolic Propellant,” Journal of the Korean Society of Propulsion Engineers, Vol. 27, No. 3, 2023, pp. 78~87. google schola Kim, K. S., Kim, Y. H., Jung, S. W., Jeong, J. Y. and Kwon, S. J., “Research Studies of Impingement Characteristics for Hypergolic Propellant,” Journal of the Korean Society of Propulsion Engineers, Vol. 23, No. 5, 2019, pp. 90~100. google schola

Related Authors

Frequently Viewed Together

Research and Review of Impinging Jet Test for Low-toxicity Hypergolic Propellant
Chungman Kim ,  Hongjae Kang ,  Kyounghwan Lee and others 1 Journal of the Korean Society of Propulsion Engineers 2023 .06
Ignition characteristics for hypergolic propellant base on H₂O₂ using doublet injector
Chungman Kim ,  Byungwoo Choi ,  Hongjae Kang and others 1 한국추진공학회 학술대회논문집 2023 .11
A Review of the Technical Development on Ionic Liquids for Hypergolic Propellants
Hongjae Kang ,  Kyounghwan Lee ,  Chungman Kim and others 1 Journal of the Korean Society of Propulsion Engineers 2022 .12
Comparison of combustion performance according to protrusion length of swirl-type single injectors Using Green Hypergolic Propellants
Wooyeol Yang ,  Jeongyeol Cha ,  Jeongseok Bang and others 3 한국추진공학회 학술대회논문집 2024 .11
Non-ignition Evaluation Method for Hypergolic Propellant Using Microreactor
Kyounghwan Lee ,  Seonghyeon Pa ,  k and others 2 Journal of the Korean Society of Propulsion Engineers 2022 .04

Recently viewed articles

The Change of Elementary Science Gifted Students' Perception about Engineers and Engineering Practices through Science and Engineering Integrated (SEI) Lessons
Han, Nuri, Nam 외 1명2018
 [Patent Litigation] 영국 대법원 “인공지능(AI)는 발명자가 될 수 없다” 최종 판결
백소민2024.02

Comments(0)

0

Write first comments.