AJ10-138

Summary

AJ10-138 is an engine model^[1].

Key Facts

• AJ10-138's image is recorded as Transtage rocket stage.jpg^[2].
• AJ10-138's instance of is recorded as engine model^[3].
• AJ10-138's manufacturer is recorded as Aerojet^[4].
• AJ10-138's subclass of is recorded as liquid propellant rocket engine^[5].
• AJ10-138's part of is recorded as AJ10^[6].
• AJ10-138's country of origin is recorded as United States^[7].
• AJ10-138's first flight is recorded as +1964-09-01T00:00:00Z^[8].
• AJ10-138's source of energy is recorded as Aerozine-50^[9].
• AJ10-138's source of energy is recorded as dinitrogen tetroxide^[10].
• AJ10-138's service retirement is recorded as +1989-09-04T00:00:00Z^[11].
• AJ10-138's used by is recorded as Transtage^[12].
• AJ10-138's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+110'}^[13].
• AJ10-138's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+35.6'}^[14].
• AJ10-138's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.53'}^[15].
• AJ10-138's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+311'}^[16].

Body

Geography

AJ10-138's part of is recorded as AJ10^[6].

Designation and Status

AJ10-138's instance of is recorded as engine model^[3].