AJ10-118K

Summary

AJ10-118K is an engine model^[1].

Key Facts

• AJ10-118K's image is recorded as Rocket0728 10.jpg^[2].
• AJ10-118K's instance of is recorded as engine model^[3].
• AJ10-118K's manufacturer is recorded as Aerojet^[4].
• AJ10-118K's manufacturer is recorded as Aerojet Rocketdyne^[5].
• AJ10-118K's subclass of is recorded as liquid propellant rocket engine^[6].
• AJ10-118K's part of is recorded as AJ10^[7].
• AJ10-118K's Commons category is recorded as AJ10-118K^[8].
• AJ10-118K's country of origin is recorded as United States^[9].
• AJ10-118K's first flight is recorded as +1982-07-16T00:00:00Z^[10].
• AJ10-118K's source of energy is recorded as Aerozine-50^[11].
• AJ10-118K's source of energy is recorded as dinitrogen tetroxide^[12].
• AJ10-118K's service retirement is recorded as +2018-09-15T00:00:00Z^[13].
• AJ10-118K's used by is recorded as Delta-K^[14].
• AJ10-118K's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.68'}^[15].
• AJ10-118K's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+98'}^[16].
• AJ10-118K's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+275'}^[17].
• AJ10-118K's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+43.38'}^[18].
• AJ10-118K's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.53'}^[19].
• AJ10-118K's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+320.5'}^[20].

Body

Geography

AJ10-118K's part of is recorded as AJ10^[7].

Physical Characteristics

AJ10-118K's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.68'}^[15].

Designation and Status

AJ10-118K's instance of is recorded as engine model^[3].