연구동향 분석

정지궤도위성의 잔여추진제량 측정방법 및 기술동향

박응식(Eungsik Park) 허환일(Hwanil Huh) 2014년

논문상세정보
인용/피인용
' 정지궤도위성의 잔여추진제량 측정방법 및 기술동향' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • 항공우주공학, 우주항법학
  • gauging(측정)
  • geostationarysatellite(정지궤도위성)
  • propellant(추진제)
  • technologystatus(기술동향)
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
495 0

0.0%

' 정지궤도위성의 잔여추진제량 측정방법 및 기술동향' 의 참고문헌

  • 저궤도 위성의 추진제 소모율 계측에 관한 고찰
    허환일 한국항공우주학회지 31 (1) : 113 ~ 121 [2003]
  • What is a Satellite?
  • Ultrasonic Flow Meter for Satellite Propellant Gauging and Ground Test Facilities
    Matthijssen, R. Van Put, P. 44th AIAA/ASME /SAE/ASEE Joint Propulsion Conference & Exhibit 21-23 [2008]
  • State-of-the art Gauging Components for Improved Propellant Management on 3-Axis Stabilized Spacecraft
    Matthijssen, R. Put, P. 42th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 9-12 [2006]
  • Satellite Propellant Gauging Analysis
    Young-Keun Chang KSAS Journal 22 (2) : 101 ~ 113 [1994]
  • Radio Frequency Mass Gauging of Propellants
    Gregory A. Zimmerli 45th AIAA Aerospace Sciences Meeting and Exhibit8-11 [2007]
  • Method for measuring the mass of liquid in a storage tank
    Brauer, L.E. US patent 5,158,362 [1992]
  • Low Gravity Propellant Gauging System for Accurate Predictions of Spacecraft End-of-Life
    Chobotov, M. V. Journal of Spacecraft and Rockets 30 (1) : 92 ~ 101 [1993]
  • Liquid Oxygen Test Results for an Optical Mass Gauge Senor
    Cyrille J. Douz 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 2-5 [2009]
  • Koreasat 3 Critical Design Review Data Package, Vol 7, book 2 of 2 propulsion
    Lockheed Martin [1997]
  • Fundamental Limitations on Low Gravity Fluid Gauging Technologies Imposed by Orbital Mission Requirements
  • Economic case for the retirement of geosynchronous communication satellites via space tugs
    Kalina K. Galabova ActaAstronautica 58 : 485 ~ 498 [2006]
  • Configuration for Propellant Gauging in Satellite
    AmitLal,B.N.Raghunandan Journal of SpacecraftandRocket 44 (1) [2007]
  • Comparative Assesment of Gauging Systems and Description of a Liquid Level Gauging Concept for a Spin Stabilised Spacecraft
    Bernhard Hufenbach Second ESA/CNES spacecraft propulsion conference : 561 ~ 570 [1997]
  • Analysis on Propellant Gauging System of KOREASAT-3 employing Thermal Mass Method
    Eung-Sik Park KSPE Journal 5 (1) [2001]
  • AIAA education series
  • ADC(Inter-AgencySpaceDebrisCoordinationCommittee) Space Debris Mitigation Guidelines
    UNCOPUOS [2002]
  • A Novel Propellant Gauging System for Use in Microgravity Based on Nuclear Magnetic Resonance
    Jeff Flowers Second European Spacecraft Propulsion Conference : 571 ~ 578 [1997]