Well folks, time for another go at Blue Origin’s first orbital launch attempt!
Blue Origin stood down from a launch attempt earlier this week due to ice forming in a purge line on an auxiliary power unit.
Scheduled for UTC | 2025-01-16 07:03 |
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Scheduled for (local) | 2025-01-16 02:03 (EST) |
Launch site | LC-36, Cape Canaveral SFS, Florida, USA |
Launch provider | Blue Origin |
Launch vehicle | New Glenn (GS1-SN001) |
Landing | Jacklyn droneship |
Payload | DarkSky-1 Blue Ring Pathfinder |
Mission success criteria | Successful insertion of New Glenn upper stage and payload into Medium Earth Orbit |
Bonus goal | Landing of booster on droneship |
Livestreams
Stream | Link |
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Blue Origin | https://www.youtube.com/watch?v=KXysNxbGdCg |
NASASpaceflight | https://www.youtube.com/watch?v=9hmOwYOO1G4 |
Spaceflight Now | https://www.youtube.com/watch?v=-27UPcCiH08 |
Space Affairs | https://www.youtube.com/watch?v=T7oyvhGApv0 |
The Launch Pad | https://www.youtube.com/watch?v=TF6SoKX1VGU |
Everyday Astronaut | https://www.youtube.com/watch?v=oqW1OjVepCk |
Stats
- 1st New Glenn mission
- 1st orbital launch attempt for Blue Origin
- 1st Blue Origin launch of 2025, 29th launch overall
Mission info
Maiden flight of the New Glenn launch vehicle. Will carry the prototype DarkSky-1 Blue Ring Pathfinder, consisting of communications array, power systems, and a flight computer affixed to a secondary payload adapter ring, remaining attached to the 2nd stage. This launch will serve as New Glenn’s first National Security Space Launch certification flight.
Previous mission (NS-28) | Next mission (NS-29)
Please post small launch updates, discussions, and questions here! Also feel free to leave feedback or suggestions for the mod team. We welcome feedback from the community!
Very, very slow liftoff. I thought there was something wrong.
Yeah, they might have dialed down the power, but it’s not like the BE-4 engines never launched before. Regardless, it made it up safe and deployed succesfully, so whatever they did worked.
Yeah, it really crawled off the pad. Thrust-to-weight-ratio can’t have been much more than 1.2 or so.