RL-10C-3

Summary

RL-10C-3 is an engine model^[1].

Key Facts

• RL-10C-3's instance of is recorded as engine model^[2].
• RL-10C-3's manufacturer is recorded as Aerojet Rocketdyne^[3].
• RL-10C-3's subclass of is recorded as RL-10C^[4].
• RL-10C-3's country of origin is recorded as United States^[5].
• RL-10C-3's source of energy is recorded as liquid oxygen^[6].
• RL-10C-3's source of energy is recorded as liquid hydrogen^[7].
• RL-10C-3's used by is recorded as Exploration Upper Stage^[8].
• RL-10C-3's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+3.16'}^[9].
• RL-10C-3's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+230.4'}^[10].
• RL-10C-3's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+108.27'}^[11].
• RL-10C-3's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.85'}^[12].
• RL-10C-3's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+460.1'}^[13].

Body

Physical Characteristics

RL-10C-3's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+3.16'}^[9].

Designation and Status

RL-10C-3's instance of is recorded as engine model^[2].