Zefiro 9A
European solid-fuel rocket stage
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Zefiro 9A
Summary
Zefiro 9A is a rocket model[1].
Key Facts
- Zefiro 9A's instance of is recorded as rocket model[2].
- Zefiro 9A's instance of is recorded as engine model[3].
- Zefiro 9A's manufacturer is recorded as Avio[4].
- Zefiro 9A's subclass of is recorded as solid-propellant rocket[5].
- Zefiro 9A's subclass of is recorded as rocket stage[6].
- Zefiro 9A's part of is recorded as Zefiro[7].
- Zefiro 9A's country of origin is recorded as Italy[8].
- Zefiro 9A's first flight is recorded as +2012-02-13T00:00:00Z[9].
- Zefiro 9A's source of energy is recorded as solid rocket propellant[10].
- Zefiro 9A's used by is recorded as Vega[11].
- Zefiro 9A's used by is recorded as Vega C[12].
- Zefiro 9A's height is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+4.12'}[13].
- Zefiro 9A's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+12000'}[14].
- Zefiro 9A's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+906'}[15].
- Zefiro 9A's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+10567'}[16].
- Zefiro 9A's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+317'}[17].
- Zefiro 9A's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.9'}[18].
- Zefiro 9A's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+295.9'}[19].
Body
Geography
Zefiro 9A's part of is recorded as Zefiro[7].
Designation and Status
Recorded instance of include rocket model[2] and engine model[3].