Gamma 201
model of British rocket engine
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Gamma 201
Summary
Gamma 201 is an engine model[1].
Key Facts
- Gamma 201's image is recorded as Black Knight tail.jpg[2].
- Gamma 201's instance of is recorded as engine model[3].
- Gamma 201's followed by is recorded as Gamma 301[4].
- Gamma 201's manufacturer is recorded as Armstrong Siddeley[5].
- Gamma 201's manufacturer is recorded as Bristol Siddeley[6].
- Gamma 201's developer is recorded as Armstrong Siddeley[7].
- Gamma 201's subclass of is recorded as rocket engine[8].
- Gamma 201's part of is recorded as Bristol Siddeley Gamma[9].
- Gamma 201's Commons category is recorded as Gamma 201[10].
- Gamma 201's country of origin is recorded as United Kingdom[11].
- +1955-00-00T00:00:00Z marks the founding of Gamma 201[12].
- Gamma 201's first flight is recorded as +1958-09-07T00:00:00Z[13].
- Gamma 201's source of energy is recorded as kerosene[14].
- Gamma 201's source of energy is recorded as hydrogen peroxide[15].
- Gamma 201's used by is recorded as Black Knight[16].
- Gamma 201's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+75'}[17].
Body
Geography
Gamma 201's part of is recorded as Bristol Siddeley Gamma[9].
Designation and Status
Gamma 201's instance of is recorded as engine model[3].
History and Context
+1955-00-00T00:00:00Z marks the founding of Gamma 201[12].