Quote from: ChrisC on 03/07/2025 03:57 pmThe troublesome laser altimeters (one inhibited by interlock, the other very noisy) were discussed at length in yesterday's news conference, and likely contributed to the wild fluctuations we were seeing. You can watch that presser here.Does anybody know which specific laser altimeters were these, like the model?
The troublesome laser altimeters (one inhibited by interlock, the other very noisy) were discussed at length in yesterday's news conference, and likely contributed to the wild fluctuations we were seeing. You can watch that presser here.
Quote from: JEF_300 on 03/14/2025 02:51 pmEvidence strongly suggests that the lander had significant, ~10 m/s, lateral velocity when landing.Agreed.Does anyone know if IM is using this tech from Advanced Navigation, or did this not pan out? Whatever they are using for altimetry and surface-rel velocity doesn't seem to be working very well. https://www.advancednavigation.com/case-studies/intuitive-machines-looks-to-advanced-navigation-laser-velocity-and-ranging-technology-for-autonomous-commercial-lunar-landings/
Evidence strongly suggests that the lander had significant, ~10 m/s, lateral velocity when landing.
There is a lot of new detail in this Eric Berger article:https://arstechnica.com/space/2025/03/athena-landed-in-a-dark-crater-where-the-temperature-was-minus-280-f/
We can do better than that. This is a composite of several stacks of images processed with different methods and combined. Look at the object right of centre. It's a disk from the bottom of the adjacent footpad which has fallen off and curled up. The image on it is outline maps of Arizona and Maryland plus some text, visible in the pre-encapsulation images. Each footpad had a different image on it.
In March 2025, our IM-2 mission landed at the southernmost location of the Moon, 5 degrees from the south pole. While in transit, our space to ground communications brought down over 8GB of data from space over our network; delivered 3 rideshare customers to trans lunar injection orbit and assisted them with ground tracking and communication; and demonstrated precision autonomous orbit operations circling the Moon for 39 orbits over a 72 hour period. While on the surface, we demonstrated the ability to manage power in thermal conditions on the south pole surface and in a crater. With the challenge of not being able to recharge the IM-2 lander solar panels post landing, the mission was still able to complete several mission and payload milestones, including downloading 500 MB of payload customer data from the lunar surface.