NASA said it would begin to roll the Artemis II rocket and spacecraft out to the launch pad at Florida's Kennedy Space Center as early as next week, and that everything is "on track" for an April ...
Morning Overview on MSN
NASA watchdog flags safety risks in SpaceX and Blue Origin moon landers
NASA’s own internal watchdog has identified schedule delays and unresolved crew safety risks in the two lunar landers meant to return astronauts to the moon’s surface. The Office of Inspector General ...
Morning Overview on MSN
NASA targets April 1 for Artemis II crewed moon mission launch
NASA has locked in April 1, 2026, as the target launch date for Artemis II, the agency’s first crewed mission around the moon in more than half a century. The four-astronaut crew will fly a ...
The Artemis II mission patch is seen on the right shoulder of the Orion Crew Survival System suits that NASA astronauts Reid Wiseman, Victor Glover ...
The mission was earlier delayed due to technical issues. Artemis II will be followed by Artemis III, which aims to support a future lunar landing planned for early 2028.
An update is coming today on NASA's Artemis 2 lunar mission to launch four astronauts on a historic journey around the moon.
NASA's moon landing program delay represents the latest in in technical, budgetary, workforce and public perception ...
NASA's Artemis II moon mission is 'go' for launch after resolving SLS rocket issues, targeting an April 1 liftoff.
After postponing launch opportunities in February and March, the agency determined that four astronauts could proceed toward the first crewed lunar journey in more than 50 years.
NASA’s approach to managing the development of crewed lunar landers for Artemis has successfully controlled costs but not schedule.
Recent engineering setbacks, specifically regarding helium system issues associated with the improper flow of helium into the Space Launch System (SLS) rocket’s upper stage, and persistent hydrogen ...
"ULA’s Centaur (with minor modifications) is the only existing in-space propulsion stage capable of meeting the SLS upper stage design parameters and performance characteristics, while also meeting ...
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