Closed MatthewGrim closed 5 years ago
Looking at the excavator results, the entire domain is accessible. This is because the design is effectively designed to survive the lunar night on its own. This implies the battery size could potentially be reduced. At the same time, the excavator now needs a solar array which may not be practical.
The demonstrator cannot access high altitude orbits. This is because we have constrained the beam to be larger than the receiver area. If this changes so the beam can be smaller, as well, it may be possible to access the higher altitude space.
With these two changes we will be up to speed with the higher power targets to where we are with Sorato and AMALIA. This is still just looking at one satellite. With more satellites, we can consider whether the excavator can be continuously powered. This may go beyond what we need for the CDF study.
So the designs as they stand can survive the lunar night for almost the entire domain. This is with the assumptions that I have currently. Changing the efficiency or the hibernation requirements may change this result.
Coming back to this issue, it seems like I have done most of what I aimed to do, and there is no need to further develop the loose ends.
This issue documents the target analysis for a lunar lander and ISRU mission demonstrator using the SPS design tool.