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Experimental investigation on No-Vent Fill (NVF) process using liquid Nitrogen

첫 페이지 보기
  • 발행기관
    한국초전도저온학회 (구 한국초전도저온공학회) 바로가기
  • 간행물
    한국초전도·저온논문지 (구 한국초전도저온공학회논문지) KCI 등재 바로가기
  • 통권
    Vol.16 No.4 (2014.12)바로가기
  • 페이지
    pp.71-77
  • 저자
    Youngcheol Kim, Mansu Seo, Donggyu Yoo, Sangkwon Jeong
  • 언어
    영어(ENG)
  • URL
    https://www.earticle.net/Article/A239911

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원문정보

초록

영어
For a long-term space mission, filling process of cryogenic liquid propellant is operated on a space vehicle in space. A vent process during transfer and filling of cryogenic propellant is needed to maintain the fuel tank pressure at a safe level due to its volatile characteristic. It is possible that both liquid and vapor phases of the cryogenic propellant are released simultaneously to outer space when the vent process occurs under low gravity environment. As a result, the existing filling process with venting not only accompanies wasting liquid propellant, but also consumes extra fuel to compensate for the unexpected momentum originated from the vent process. No-Vent Fill (NVF) method, a filling procedure without a venting process of cryogenic liquid propellant, is an attractive technology to perform a long-term space mission. In this paper, the preliminary experimental results of the NVF process are described. The experimental set-up consists of a 9-liter cryogenic liquid receiver tank and a supply tank. Liquid nitrogen (LN2) is used to simulate the behavior of cryogenic propellant. The whole situation in the receiver tank during NVF is monitored. The major experimental parameter in the experiment is the mass flow rate of the liquid nitrogen. The experimental results demonstrate that as the mass flow rate is increased, NVF process is conducted successfully. The quality and the inlet temperature of the injected LN2 are affected by the mass flow rate. These parameters determine success of NVF.

목차

Abstract
 1. INTRODUCTION
 2. EXPERIMENT
  2.1. Configuration of a NVF experiment apparatus
  2.2. NVF experiment process and the conditions
  2.3. Confirmation experiment for the inlet condition
 3. RESULTS
  3.1. NVF experiment results
  3.2. Results of the confirmation experiment
 4. CONCLUSIONS
 ACKNOWLEDGMENT
 REFERENCES

키워드

No-vent fill (NVF) Cryogenic propellants Low gravity environment

저자

  • Youngcheol Kim [ Korea Advanced Institute of Science and Technology, Daejeon, Korea ] Corresponding author
  • Mansu Seo [ Korea Advanced Institute of Science and Technology, Daejeon, Korea ]
  • Donggyu Yoo [ Korea Advanced Institute of Science and Technology, Daejeon, Korea ]
  • Sangkwon Jeong [ Korea Advanced Institute of Science and Technology, Daejeon, Korea ]

참고문헌

자료제공 : 네이버학술정보

간행물 정보

발행기관

  • 발행기관명
    한국초전도저온학회 (구 한국초전도저온공학회) [The Korean Society of Superconductivity and Cryogenics (KSSC)]
  • 설립연도
    1998
  • 분야
    공학>전기공학
  • 소개
    21세기 핵심기술인 초전도공학과 저온공학분야의 기술 수준을 향상시키고, 선진 외국의 관련 학회와의 국제 교류 뿐만 아니라 이 분야에서 산.학.연의 학술활동 및 기술교류의 구심점으로의 그 역할을 성실히 수행하고자 한다.

간행물

  • 간행물명
    한국초전도·저온논문지 (구 한국초전도저온공학회논문지) [Progress in Superconductivity and Cryogenics]
  • 간기
    계간
  • pISSN
    1229-3008
  • eISSN
    2287-6251
  • 수록기간
    1999~2026
  • 등재여부
    KCI 등재,SCOPUS
  • 십진분류
    KDC 427 DDC 537

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