A study on Propulsion Fuel consumption rate for orbit maintenance of LEO

  • 정도희 (조선대학교 우주항공공학과) ;
  • 공창덕 (조선대학교 우주항공공학과)
  • Published : 2000.11.01


For low Earth orbit, the atmosphere causes orbit altitude to decrease, If this decrease is not corrected by the satellite propulsive unit, the orbit decoys continuously unit reaches the dense atmosphere and satellite life ends. If active orbit maintenance is mode by satellite propulsive unit then fuel consumption is necessary, which must be considered in the satellite design. Especially interesting is the method for evaluating the fuel consumption role for maintenance of elliptical orbit developed in this paper.(omitted)