AJ10-190

Summary

AJ10-190 is an engine model^[1].

Key Facts

• AJ10-190's instance of is recorded as engine model^[2].
• AJ10-190's manufacturer is recorded as Aerojet^[3].
• AJ10-190's subclass of is recorded as liquid propellant rocket engine^[4].
• AJ10-190's part of is recorded as AJ10^[5].
• AJ10-190's country of origin is recorded as United States^[6].
• AJ10-190's first flight is recorded as +1981-00-00T00:00:00Z^[7].
• AJ10-190's source of energy is recorded as hypergolic propellant^[8].
• AJ10-190's significant event is recorded as contract^[9].
• AJ10-190's significant event is recorded as development^[10].
• AJ10-190's significant event is recorded as certification^[11].
• AJ10-190's significant event is recorded as maiden flight^[12].
• AJ10-190's used by is recorded as Space Shuttle Orbital Maneuvering System^[13].
• AJ10-190's used by is recorded as European Service Module^[14].
• AJ10-190's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q174728', 'amount': '+195'}^[15].
• AJ10-190's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+118'}^[16].
• AJ10-190's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+27'}^[17].
• AJ10-190's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q174728', 'amount': '+117'}^[18].
• AJ10-190's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+316'}^[19].

Body

Geography

AJ10-190's part of is recorded as AJ10^[5].

Physical Characteristics

AJ10-190's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q174728', 'amount': '+195'}^[15].

Designation and Status

AJ10-190's instance of is recorded as engine model^[2].