XLR-89-5
American rocket engine
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XLR-89-5
Summary
Key Facts
- XLR-89-5's manufacturer is recorded as Rocketdyne[1].
- XLR-89-5 is a type of rocket engine[2].
- XLR-89-5's country of origin is recorded as United States[3].
- XLR-89-5's source of energy is recorded as liquid oxygen[4].
- XLR-89-5's source of energy is recorded as RP-1[5].
- XLR-89-5's service entry is recorded as +1958-00-00T00:00:00Z[6].
- XLR-89-5's used by is recorded as SM-65D Atlas[7].
- XLR-89-5's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+643'}[8].
- XLR-89-5's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+758.7'}[9].
- XLR-89-5's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.45'}[10].
Body
Definition and Type
XLR-89-5 is a type of rocket engine[2].
Use and Application
XLR-89-5's used by is recorded as SM-65D Atlas[7].