Vulcain 2.1

Summary

Vulcain 2.1 is an engine model^[1].

Key Facts

• Vulcain 2.1's instance of is recorded as engine model^[2].
• Vulcain 2.1's follows is recorded as Vulcain 2^[3].
• Vulcain 2.1's manufacturer is recorded as Safran Aircraft Engines^[4].
• Vulcain 2.1's manufacturer is recorded as Avio^[5].
• Vulcain 2.1's manufacturer is recorded as GKN^[6].
• Vulcain 2.1's subclass of is recorded as cryogenic rocket engine^[7].
• Vulcain 2.1's part of is recorded as Vulcain^[8].
• Vulcain 2.1's first flight is recorded as +2024-07-09T00:00:00Z^[9].
• Vulcain 2.1's source of energy is recorded as liquid oxygen^[10].
• Vulcain 2.1's source of energy is recorded as liquid hydrogen^[11].
• Vulcain 2.1's used by is recorded as LLPM H140^[12].
• Vulcain 2.1's height is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+3.6'}^[13].
• Vulcain 2.1's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+1371'}^[14].
• Vulcain 2.1's uses is recorded as gas-generator cycle^[15].
• Vulcain 2.1's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.1'}^[16].
• Vulcain 2.1's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+432'}^[17].

Body

Geography

Vulcain 2.1's part of is recorded as Vulcain^[8].

Designation and Status

Vulcain 2.1's instance of is recorded as engine model^[2].