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ORBITER-FORUM will be temporarily closed at 2026-07-23 18:00 UTC while we complete some OF maintenance tasks. The amount of downtime is expected to take up to one hour, but probably less.
This was Yusaku Maezawa's exact original plan up until the first flight of Falcon Heavy back in 2018. He and one other person will ride a Crew Dragon on a circumlunar trajectory. Post-Tesla, he was most likely convinced to change his mind to ride on Starship instead when the Falcon Heavy isn't...
I think they need to be defined as both CHILD and PARENT attachments since most likely the arm must move anywhere the station like the Canadarm2 is doing at the ISS
The concept arts highly indicate that Starlab is going to be launched in one piece, i.e. its propulsion and habitat modules are bolted together permanently
Except for Axiom, which will co-orbit the ISS until the latter is decomissioned, we know virtually nothing about the specific orbital parameters for either Orbital Reef, Haven-1, or Starlab. All we know is that they are going to be placed in LEO
I'd understood why Gateway is planned to be placed in high lunar orbit than a low one. Less time for communication blackouts by simply going behind the Moon on Earth's perspective, and (pure speculation here) they also want to have crewed landings on the Far Side sometime in the future
Apollo had 5 test flights (2 suborbital, 2 HEO, 1 LEO) dedicated in testing its heat shield performance before Apollo 8, while Orion had only EFT-1 doing it before Artemis 1. I think even if Apollo engineers had less experience in terms of actual spaceflight time, they understood more of how...
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