AJ10-118F

Summary

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

Key Facts

• AJ10-118F's instance of is recorded as engine model^[2].
• AJ10-118F's manufacturer is recorded as Aerojet^[3].
• AJ10-118F's subclass of is recorded as liquid propellant rocket engine^[4].
• AJ10-118F's part of is recorded as AJ10^[5].
• AJ10-118F's country of origin is recorded as United States^[6].
• AJ10-118F's source of energy is recorded as red fuming nitric acid^[7].
• AJ10-118F's source of energy is recorded as 1,1-dimethylhydrazine^[8].
• AJ10-118F's used by is recorded as Delta 0100^[9].
• AJ10-118F's used by is recorded as Delta 1000^[10].
• AJ10-118F's used by is recorded as N-II^[11].
• AJ10-118F's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+95'}^[12].
• AJ10-118F's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+41.4'}^[13].
• AJ10-118F's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.4'}^[14].
• AJ10-118F's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+306'}^[15].

Body

Geography

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

Designation and Status

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