Atlas MA-2
American rocket stage
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Atlas MA-2
Summary
Key Facts
- Atlas MA-2's subclass of is recorded as rocket stage[1].
- Atlas MA-2's part of is recorded as Atlas[2].
- Atlas MA-2's country of origin is recorded as United States[3].
- Atlas MA-2's powered by is recorded as XLR-89-5[4].
- Atlas MA-2's source of energy is recorded as liquid oxygen[5].
- Atlas MA-2's source of energy is recorded as RP-1[6].
- Atlas MA-2's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+3050'}[7].
- Atlas MA-2's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+1517.42'}[8].
- Atlas MA-2's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+4.9'}[9].