Gamma 2

Summary

Gamma 2 is an engine model^[1].

Key Facts

• Gamma 2's image is recorded as Black Arrow 2nd stage engine.jpg^[2].
• Gamma 2's instance of is recorded as engine model^[3].
• Gamma 2's follows is recorded as Gamma 301^[4].
• Gamma 2's manufacturer is recorded as Bristol Siddeley^[5].
• Gamma 2's subclass of is recorded as rocket engine^[6].
• Gamma 2's part of is recorded as Bristol Siddeley Gamma^[7].
• Gamma 2's Commons category is recorded as Gamma 2^[8].
• Gamma 2's Commons category is recorded as Bristol Siddeley Gamma^[9].
• Gamma 2's country of origin is recorded as United Kingdom^[10].
• Gamma 2's first flight is recorded as +1969-06-29T00:00:00Z^[11].
• Gamma 2's source of energy is recorded as kerosene^[12].
• Gamma 2's source of energy is recorded as hydrogen peroxide^[13].
• Gamma 2's total produced is recorded as {'unit': '1', 'amount': '+4'}^[14].
• Gamma 2's used by is recorded as Black Arrow^[15].
• Gamma 2's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+173'}^[16].
• Gamma 2's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+68.2'}^[17].
• Gamma 2's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+64.6'}^[18].
• Gamma 2's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.37'}^[19].
• Gamma 2's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+265'}^[20].
• Gamma 2's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+251'}^[21].

Body

Geography

Gamma 2's part of is recorded as Bristol Siddeley Gamma^[7].

Designation and Status

Gamma 2's instance of is recorded as engine model^[3].