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달 궤도 진입 목표값 변화에 따른 궤도요소 변화 연구
논문 개요
| 기관명 | NDSL |
|---|---|
| 저널명 | 항공우주시스템공학회지 = Journal of aerospace system engineering |
| ISSN | 1976-6300, |
| ISBN |
논문저자 및 소속기관 정보
| 저자(한글) | 최수진,김인규,문상만,민승용,류동영 |
|---|---|
| 저자(영문) | |
| 소속기관 | |
| 소속기관(영문) | |
| 출판인 | |
| 간행물 번호 | |
| 발행연도 | 2015-01-01 |
| 초록 | Korea Aerospace Research Institute(here after KARI) has a plan to launch experimental lunar orbiter in 2018, and lunar orbiter and lander in 2020. There are several ways to go to the moon. Which one is direct transfer trajectory and another one is phasing loop transfer trajectory and the other one is WSB trajectory. Regardless of the transfer trajectories, LOI maneuver is the most important maneuver of all mission sequences because if this burn is failed, it is too difficult to get into the lunar orbit in the future. This paper describes first LOI target value of foreign lunar orbiters and analyzes orbital variations of experimental lunar orbiter according to various target values. By analyzing the variation of orbiter parameter after first LOI, proper orbital period for LOI target value are recommended to meet the inclination, apoapsis and periapsis altitude constraints. |
| 원문URL | http://click.ndsl.kr/servlet/OpenAPIDetailView?keyValue=03553784&target=NART&cn=JAKO201506838217801 |
| 첨부파일 |
추가정보
| 과학기술표준분류 | |
|---|---|
| ICT 기술분류 | |
| DDC 분류 | |
| 주제어 (키워드) | Lunar Orbit Insertion,Lunar Orbiter,Orbital elements, lt,TEX gt,${ Delta}V$ lt,/TEX gt,. Target Value,Inclination,Eccentricity,Burn Duration |