As I understand it this means the mission will take quite a bit more time than "usual" but save a lot of power.
[0] I'm on mobile, but this looks like a decent representation https://twitter.com/TitaniumSV5/status/1695724234339954779?t...
As I understand it this means the mission will take quite a bit more time than "usual" but save a lot of power.
[0] I'm on mobile, but this looks like a decent representation https://twitter.com/TitaniumSV5/status/1695724234339954779?t...
Official reasons given is it allows reduction of structural margins, physical interferences and tipover risks on inclined surfaces, which seem to make sense. Maybe it's just me that it looks a bit like someone had to have a spacecraft that lands like the Space Shuttle with engines pointing back.
1: https://www.isas.jaxa.jp/feature/forefront/files/201912_1.jp...
Descend vertically to keep from having to worry about balancing a bunch of thrusters.
Then, tip over, hopefully in the right orientation and gently enough to not blow up.
It starts sort of the same way, but then it uses the moon's own attraction to project itself much further out and then come back approaching the moon in a different way.
In comparison, the Chandrayaan and Mars orbiter missions approached their target only once. And the insertion was also somewhat drastic, with a long retro-burn.
I wouldn't be surprised if he expressed doubt over the Moon landings considering that he was also the one to push the absurd claim that the hole that had been drilled into a Soyuz was sabotage done by a space-crazed American female astronaut.