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Rocketdyne MA-2 Atlas D propulsion system

The integrated Rocketdyne MA-2 propulsion system used by the Atlas D (SM-65D) ICBM and its early space-launch derivatives. The exact integrated boundary is retained because the consulted primary sources establish the MA-2 system and its stage-and-a-half architecture, but do not consistently establish one component suffix set across the ICBM and Mercury installations.

Identity

Aliases
MA-2MA-2 drive systemAtlas D MA-2
Domains
spaceflight
Identity Level
integrated-system
Kind
integrated-propulsion-system
Name
Rocketdyne MA-2 Atlas D propulsion system
Status
historical

Details

Description
The integrated Rocketdyne MA-2 propulsion system used by the Atlas D (SM-65D) ICBM and its early space-launch derivatives. The exact integrated boundary is retained because the consulted primary sources establish the MA-2 system and its stage-and-a-half architecture, but do not consistently establish one component suffix set across the ICBM and Mercury installations.
Propellants
RP-1liquid oxygen
Retirement Date
1965
Service Entry Date
1959

Links

Assets & Meta

Creation Time
August 1, 2026 at 16:56:33 UTC
Updated Time
August 1, 2026 at 16:56:33 UTC

Other

Sources
Rocketdyne MA-2 Atlas D propulsion system - AeroVia