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SpaceX Crew-8 was the eighth crewed operational NASA Commercial Crew flight and the 13th overall crewed orbital flight of a Crew Dragon spacecraft. The mission launched on 4 March 2024. The Crew-8 mission transported four crew members to the International Space Station (ISS).
December 20: The Boeing Orbital Flight Test, an uncrewed flight test of the Boeing Starliner crew spacecraft, is successfully launched but experiences several technical issues in orbit related to an erroneously configured mission timer. The planned docking attempt to the ISS was called off and the spacecraft landed in New Mexico two days later ...
Docking or Berthing Yes Used on the ISS International Docking Adapter, SpaceX Dragon 2, Boeing Starliner and future vehicles. Circular transfer passage diameter is 800 mm (31 in). [28] The International Berthing and Docking Mechanism (IBDM) is an implementation of IDSS to be used on European Space Agency spacecraft. [29]
NASA astronaut Nick Hague and Roscosmos cosmonaut Aleksandr Gorbunov boarded the ISS shortly after the Dragon capsule docked at the station at 2130 GMT, NASA said in a post on X. The SpaceX Crew-9 ...
Astronauts aboard the International Space Station plan to find a new docking port for a SpaceX Dragon in order to make way for an uncrewed NASA vehicle on a resupply mission.. The Dragon ...
A SpaceX crew on a rescue mission have arrived at the International Space Station, but it will still be some time before stranded Boeing Starliner astronauts Butch Wilmore and Suni Williams can ...
SpaceX Crew-9 is the ninth operational NASA Commercial Crew Program flight and the 15th crewed orbital flight of a Crew Dragon spacecraft. Originally scheduled to launch a crew of four to the International Space Station (ISS) in mid-August 2024, the mission was delayed by more than a month due to technical issues with the Boeing Starliner Calypso spacecraft that was docked at the ISS for the ...
In April 2012, NASA funded a study to determine if a less complex docking system could be used as the NASA Docking System that both met the international community's desire for a narrower soft capture system ring width, as well as providing the ISS a simpler active docking system compared to the then-planned design. [10]