RL-10A-3

Summary

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

Key Facts

• RL-10A-3's instance of is recorded as engine model^[2].
• RL-10A-3's manufacturer is recorded as Pratt & Whitney^[3].
• RL-10A-3's subclass of is recorded as RL-10A^[4].
• RL-10A-3's country of origin is recorded as United States^[5].
• RL-10A-3's first flight is recorded as +1967-00-00T00:00:00Z^[6].
• RL-10A-3's source of energy is recorded as liquid oxygen^[7].
• RL-10A-3's source of energy is recorded as liquid hydrogen^[8].
• RL-10A-3's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.49'}^[9].
• RL-10A-3's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+131'}^[10].
• RL-10A-3's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+65.60'}^[11].
• RL-10A-3's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.53'}^[12].
• RL-10A-3's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+444'}^[13].

Body

Physical Characteristics

RL-10A-3's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.49'}^[9].

Designation and Status

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