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TECHNICAL PAPERS : An Investigation on the Propellant Consumption Rate Gauged from the Low-Earth-Orbit Spacecraft

기술논문 : 저궤도 위성의 추진제 소모율 계측에 관한 고찰

  • 김인태 (충남대학교 항공우주공학과 대학원) ;
  • 허환일 (충남대학교 항공우주공학과) ;
  • 김정수 (한국항공우주연구원)
  • Published : 2003.02.01

Abstract

During the mission operation time, it is very important to estimate the spacecraft propellant remaining as accurately as possible. This is because the quantity of propellant is related directly to how long the satellite can be operated ín orbit. There are two different methods for spacecraft propellant gauging; the PVT method and the book-keeping method. This paper describes the characteristics and applications of these methods using the flight operation data of KOMPSAT-1. Additionally, propellant consumption rates in delta-V maneuvering and each attitude control submode are analyzed according to spacecraft operation modes. The earth search submode shows the highest propellant consumption rate.

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Cited by

  1. Residual Propellant Gauging Methods for Geostationary Satellites and Recent Technology Status vol.42, pp.10, 2014, https://doi.org/10.5139/JKSAS.2014.42.10.870