AJ10-137

Summary

AJ10-137 is an engine model^[1].

Key Facts

• AJ10-137's image is recorded as Chambre-de-combustion-du-moteur-AJ10-137.jpg^[2].
• AJ10-137's instance of is recorded as engine model^[3].
• AJ10-137's manufacturer is recorded as Aerojet^[4].
• AJ10-137's subclass of is recorded as liquid propellant rocket engine^[5].
• AJ10-137's part of is recorded as AJ10^[6].
• AJ10-137's Commons category is recorded as AJ10-137^[7].
• AJ10-137's country of origin is recorded as United States^[8].
• AJ10-137's first flight is recorded as +1966-02-26T00:00:00Z^[9].
• AJ10-137's source of energy is recorded as Aerozine-50^[10].
• AJ10-137's source of energy is recorded as dinitrogen tetroxide^[11].
• AJ10-137's service retirement is recorded as +1975-07-16T00:00:00Z^[12].
• AJ10-137's used by is recorded as Apollo Service Module^[13].
• AJ10-137's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+91.19'}^[14].
• AJ10-137's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+314.5'}^[15].

Body

Geography

AJ10-137's part of is recorded as AJ10^[6].

Designation and Status

AJ10-137's instance of is recorded as engine model^[3].