Atlas booster engine, XLR-89-NA-3, installed as one of two outboard booster engines to propel the Atlas missile at launch, had a thrust of 165,000 pounds with a burn time of 270 seconds.

ID: 117 | This file appears in: Sands Space History Center
Atlas booster engine, XLR-89-NA-3, installed as one of two outboard booster engines to propel the Atlas missile at launch, had a thrust of 165,000 pounds with a burn time of 270 seconds.
Source: Sands Space History Center
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Sands Space History Center
"Atlas booster engine, XLR-89-NA-3, installed as one of two outboard booster engines to propel the Atlas missile at launch, had a thrust of 165,000 pounds with a burn time of 270 seconds. " appears in: Sands Space History Center