Reachable set analysis of practical trans-lunar orbit via a retrograde semi-analytic model
Abstract Different from the Apollo flight mode, a safer trans-lunar flight mode for the crews is preferred. The previous-arrived lunar module rendezvouses with the crew exploration vehicle at a low lunar destination orbit, and then the crews ride the lunar module to descend the lunar surface samplin...
Main Authors: | Bo-yong He, Sheng-gang Wu, Heng-nian Li |
---|---|
Format: | Article |
Language: | English |
Published: |
SpringerOpen
2023-03-01
|
Series: | Earth, Planets and Space |
Subjects: | |
Online Access: | https://doi.org/10.1186/s40623-023-01782-y |
Similar Items
-
Development of Precise Lunar Orbit Propagator and Lunar Polar Orbiter’s Lifetime Analysis
by: Young-Joo Song, et al.
Published: (2010-06-01) -
Development of Kinematic Ephemeris Generator for Korea Pathfinder Lunar Orbiter (KPLO)
by: Min-Sup Song, et al.
Published: (2020-09-01) -
Burn Delay Analysis of the Lunar Orbit Insertion for Korea Pathfinder Lunar Orbiter
by: Jonghee Bae, et al.
Published: (2017-12-01) -
Observational Arc-Length Effect on Orbit Determination for Korea Pathfinder Lunar Orbiter in the Earth-Moon Transfer Phase Using a Sequential Estimation
by: Kim, Youngrok, et al.
Published: (2019-12-01) -
A New View of the Lunar South Pole from the Lunar Orbiter Laser Altimeter (LOLA)
by: Michael K. Barker, et al.
Published: (2023-01-01)