RL-10C-1-1

Summary

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

Key Facts

• RL-10C-1-1's instance of is recorded as engine model^[2].
• RL-10C-1-1's manufacturer is recorded as Aerojet Rocketdyne^[3].
• RL-10C-1-1's subclass of is recorded as RL-10C^[4].
• RL-10C-1-1's country of origin is recorded as United States^[5].
• RL-10C-1-1's source of energy is recorded as liquid oxygen^[6].
• RL-10C-1-1's source of energy is recorded as liquid hydrogen^[7].
• RL-10C-1-1's used by is recorded as Centaur V^[8].
• RL-10C-1-1's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.46'}^[9].
• RL-10C-1-1's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+188.2'}^[10].
• RL-10C-1-1's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+105.98'}^[11].
• RL-10C-1-1's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.57'}^[12].
• RL-10C-1-1's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+453.8'}^[13].

Body

Physical Characteristics

RL-10C-1-1's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.46'}^[9].

Designation and Status

RL-10C-1-1's instance of is recorded as engine model^[2].