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Bristol Aeroplane Co Ltd. Stress Department: Olympus 102 Avro jet pipe characteristics...
Catalogue reference: PA1716/5/11/2/154
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This record is a file about the Bristol Aeroplane Co Ltd. Stress Department: Olympus 102 Avro jet pipe characteristics... dating from 16 January 1956.
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Full description and record details
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Reference (The unique identifier to the record described, used to order and refer to it)
- PA1716/5/11/2/154
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Title (The name of the record)
- Bristol Aeroplane Co Ltd. Stress Department: Olympus 102 Avro jet pipe characteristics Airflow function vs thrust
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Date (When the record was created)
- 16 January 1956
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Description (What the record is about)
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Issued by the Performance & Aerodynamic Department. Engine Division Filton Bristol. Drawn by DWL. 27' diameter Avro pipe; 22.389' diameter inclined flight nozzle. TED.6987. This curve is consistent with TED.6091 Issue 2. Engine No.10132 Build 2 No,2.GP. 26.7555. TED.6987
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Held by (Who holds the record)
- Coventry Archives & Research Centre
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Language (The language of the record)
- English
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Physical description (The amount and form of the record)
- 1 Item
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Record URL
- https://beta.nationalarchives.gov.uk/catalogue/id/e023d496-5d87-485e-ab8c-eef6add3471c/
Series information
PA1716/5/11/2
Bristol Gas Turbines: Olympus stress reports & calculations for all models
See the series level description for more information about this record.
Catalogue hierarchy
This record is held at Coventry Archives & Research Centre
Within the fonds: PA1716
Rolls-Royce Heritage Trust, Coventry Branch - Records of Armstrong Siddeley, Bristol...
Within the sub-fonds: PA1716/5
Armstrong Siddeley/Bristol Siddeley & Rolls-Royce Gas Turbines
Within the sub-sub-fonds: PA1716/5/11
Olympus Engine
Within the series: PA1716/5/11/2
Bristol Gas Turbines: Olympus stress reports & calculations for all models
You are currently looking at the file: PA1716/5/11/2/154
Bristol Aeroplane Co Ltd. Stress Department: Olympus 102 Avro jet pipe characteristics Airflow function vs thrust