AJ10-118

Summary

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

Key Facts

• AJ10-118's instance of is recorded as engine model^[2].
• AJ10-118's manufacturer is recorded as Aerojet^[3].
• AJ10-118's subclass of is recorded as liquid propellant rocket engine^[4].
• AJ10-118's part of is recorded as AJ10^[5].
• AJ10-118's country of origin is recorded as United States^[6].
• AJ10-118's source of energy is recorded as white fuming nitric acid^[7].
• AJ10-118's source of energy is recorded as 1,1-dimethylhydrazine^[8].
• AJ10-118's used by is recorded as Delta A^[9].
• AJ10-118's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+90'}^[10].
• AJ10-118's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+33.8'}^[11].
• AJ10-118's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+0.84'}^[12].
• AJ10-118's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+271'}^[13].

Body

Geography

AJ10-118's part of is recorded as AJ10^[5].

Designation and Status

AJ10-118's instance of is recorded as engine model^[2].