Gamma 8

Summary

Gamma 8 is an engine model^[1].

Key Facts

• Gamma 8's image is recorded as Gamma 8 rocket engine on Black Arrow 1st stage.jpg^[2].
• Gamma 8's instance of is recorded as engine model^[3].
• Gamma 8's follows is recorded as Gamma 301^[4].
• Gamma 8's manufacturer is recorded as Bristol Siddeley^[5].
• Gamma 8's subclass of is recorded as rocket engine^[6].
• Gamma 8's part of is recorded as Bristol Siddeley Gamma^[7].
• Gamma 8's Commons category is recorded as Gamma 8^[8].
• Gamma 8's country of origin is recorded as United Kingdom^[9].
• Gamma 8's first flight is recorded as +1969-06-29T00:00:00Z^[10].
• Gamma 8's source of energy is recorded as kerosene^[11].
• Gamma 8's source of energy is recorded as hydrogen peroxide^[12].
• Gamma 8's total produced is recorded as {'unit': '1', 'amount': '+4'}^[13].
• Gamma 8's used by is recorded as Black Arrow^[14].
• Gamma 8's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+342'}^[15].
• Gamma 8's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+234.8'}^[16].
• Gamma 8's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+222.4'}^[17].
• Gamma 8's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.98'}^[18].
• Gamma 8's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+265'}^[19].
• Gamma 8's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+251'}^[20].

Body

Geography

Gamma 8's part of is recorded as Bristol Siddeley Gamma^[7].

Designation and Status

Gamma 8's instance of is recorded as engine model^[3].