Zefiro 40

Summary

Zefiro 40 is a rocket model^[1].

Key Facts

• Zefiro 40's instance of is recorded as rocket model^[2].
• Zefiro 40's instance of is recorded as engine model^[3].
• Zefiro 40's manufacturer is recorded as Avio^[4].
• Zefiro 40's subclass of is recorded as solid-propellant rocket^[5].
• Zefiro 40's subclass of is recorded as rocket stage^[6].
• Zefiro 40's part of is recorded as Zefiro^[7].
• Zefiro 40's country of origin is recorded as Italy^[8].
• Zefiro 40's first flight is recorded as +2022-07-13T00:00:00Z^[9].
• Zefiro 40's source of energy is recorded as solid rocket propellant^[10].
• Zefiro 40's used by is recorded as Vega C^[11].
• Zefiro 40's height is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+8.07'}^[12].
• Zefiro 40's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+40477'}^[13].
• Zefiro 40's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+3006'}^[14].
• Zefiro 40's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+36239'}^[15].
• Zefiro 40's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+1304'}^[16].
• Zefiro 40's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.4'}^[17].
• Zefiro 40's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+293.5'}^[18].

Body

Geography

Zefiro 40's part of is recorded as Zefiro^[7].

Designation and Status

Recorded instance of include rocket model^[2] and engine model^[3].