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Antares IIB

Antares IIB is the exact solid third-stage motor used in the Scout D-1 configuration, retained separately from Antares IIIA and other Antares variants. NASA's Scout characteristics table lists 93.05 kN average thrust and a nominal burn time of 37 seconds for the D-1 Antares IIB stage. NASA's Scout Nozzle Data Book documents the IIB nozzle and its limited alternate use in the Scout third stage; no exact canonical AeroVia company record is available for the historical ABL/Hercules contractor boundary, so developer and manufacturer links remain empty. NASA records the final Scout launch on 5 August 1994, so this Scout-specific motor designation is marked retired.

Identity

Aliases
Antares 2BScout D-1 third-stage Antares IIB
Domains
spaceflight
Identity Level
variant
Kind
solid-rocket-motor
Name
Antares IIB
Status
retired

Details

Description
Antares IIB is the exact solid third-stage motor used in the Scout D-1 configuration, retained separately from Antares IIIA and other Antares variants. NASA's Scout characteristics table lists 93.05 kN average thrust and a nominal burn time of 37 seconds for the D-1 Antares IIB stage. NASA's Scout Nozzle Data Book documents the IIB nozzle and its limited alternate use in the Scout third stage; no exact canonical AeroVia company record is available for the historical ABL/Hercules contractor boundary, so developer and manufacturer links remain empty. NASA records the final Scout launch on 5 August 1994, so this Scout-specific motor designation is marked retired.
Propellants
solid composite propellant
Rocket Specs
Burn Time S
37
Sea Level Thrust Kn
93.05

Links

Assets & Meta

Creation Time
August 1, 2026 at 16:01:39 UTC
Updated Time
August 21, 2026 at 01:17:41 UTC

Other

Sources