AJ10-220

Summary

AJ10-220 is an engine model^[1].

Key Facts

• AJ10-220's instance of is recorded as engine model^[2].
• AJ10-220's manufacturer is recorded as Aerojet Rocketdyne^[3].
• AJ10-220's subclass of is recorded as liquid propellant rocket engine^[4].
• AJ10-220's part of is recorded as AJ10^[5].
• AJ10-220's has use is recorded as reaction control system^[6].
• AJ10-220's country of origin is recorded as United States^[7].
• AJ10-220's source of energy is recorded as hypergolic propellant^[8].
• AJ10-220's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q174728', 'amount': '+19.0'}^[9].
• AJ10-220's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+1.95'}^[10].
• AJ10-220's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q12438', 'amount': '+65.4'}^[11].
• AJ10-220's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q12438', 'amount': '+62.3'}^[12].
• AJ10-220's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q174728', 'amount': '+7.3'}^[13].
• AJ10-220's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+285'}^[14].

Body

Geography

AJ10-220's part of is recorded as AJ10^[5].

Physical Characteristics

AJ10-220's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q174728', 'amount': '+19.0'}^[9].

Designation and Status

AJ10-220's instance of is recorded as engine model^[2].