The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan
One candidate of the post- HINODE Solar Observation Mission targets on the observation of the high latitude region of the Sun, which requires the injection of the spacecraft into the orbit largely inclined with the ecliptic plane. In the previous workshops, we reported a mission design result based on a sequential application of EDVEGA procedure. Reported in this presentation are the results of analyses focusing on the sensitivity of the design parameters to the trajectory design.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
Sensitivity Analysis on the Trajectory Design of the Solar Polar Region Observation Mission (Solar Electric Propulsion Option)
