Gamma 301

Summary

Gamma 301 is an engine model^[1].

Key Facts

• Gamma 301's instance of is recorded as engine model^[2].
• Gamma 301's follows is recorded as Gamma 201^[3].
• Gamma 301's followed by is recorded as Gamma 2^[4].
• Gamma 301's followed by is recorded as Gamma 8^[5].
• Gamma 301's manufacturer is recorded as Armstrong Siddeley^[6].
• Gamma 301's manufacturer is recorded as Bristol Siddeley^[7].
• Gamma 301's developer is recorded as Armstrong Siddeley^[8].
• Gamma 301's subclass of is recorded as rocket engine^[9].
• Gamma 301's part of is recorded as Bristol Siddeley Gamma^[10].
• Gamma 301's Commons category is recorded as Gamma 301^[11].
• Gamma 301's country of origin is recorded as United Kingdom^[12].
• +1957-00-00T00:00:00Z marks the founding of Gamma 301^[13].
• Gamma 301's first flight is recorded as +1962-08-24T00:00:00Z^[14].
• Gamma 301's source of energy is recorded as kerosene^[15].
• Gamma 301's source of energy is recorded as hydrogen peroxide^[16].
• Gamma 301's used by is recorded as Black Knight^[17].
• Gamma 301's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+75'}^[18].

Body

Geography

Gamma 301's part of is recorded as Bristol Siddeley Gamma^[10].

Designation and Status

Gamma 301's instance of is recorded as engine model^[2].

History and Context

+1957-00-00T00:00:00Z marks the founding of Gamma 301^[13].