Combustion chamber for gas turbine

Combustion chamber for gas turbine

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Combustion chamber for Rolls Royce "Derwent 1" gas turbine (sectioned)

Details

Category:
Aircraft Propulsion
Object Number:
1982-865
Measurements:
overall: 600 mm x 90 mm x 180 mm,
type:
combustion chamber
credit:
Cranfield Institute of Technology