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Astrobotic Xodiac-B

Xodiac-B is a planned reusable hover testbed derived from Xodiac for kerosene-fueled rotating-detonation engines in the 1,000-lbf thrust class. Announced design targets include 500 m altitude and 300 m downrange translation. Its development award supports flight validation of advanced propulsion.

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Identity

Aliases
Xodiac-B
Family Name
Xodiac
Full Name
Astrobotic Xodiac-B
Roles
researchexperimentaltechnology_demonstratorlander
Status
development
Type
rocket
Variant Name
B

Details

Description
Xodiac-B is a planned reusable hover testbed derived from Xodiac for kerosene-fueled rotating-detonation engines in the 1,000-lbf thrust class. Announced design targets include 500 m altitude and 300 m downrange translation. Its development award supports flight validation of advanced propulsion.
Operator
Parent Vehicle Family
Rocket Specs
Reusability
fully_reusable

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Creation Time
October 29, 2026 at 15:52:59 UTC
Updated Time
October 29, 2026 at 15:52:59 UTC