File
Bristol Aeroplane Co Ltd. Stress Department: Olympus 104 jet pipe characteristics
Catalogue reference: PA1716/5/11/2/155
What’s it about?
This record is a file about the Bristol Aeroplane Co Ltd. Stress Department: Olympus 104 jet pipe characteristics dating from 14 November 1957.
Access information is unavailable
Sorry, information for accessing this record is currently unavailable online. Please try again later.
Full description and record details
-
Reference (The unique identifier to the record described, used to order and refer to it)
- PA1716/5/11/2/155
-
Title (The name of the record)
- Bristol Aeroplane Co Ltd. Stress Department: Olympus 104 jet pipe characteristics
-
Date (When the record was created)
- 14 November 1957
-
Description (What the record is about)
-
Issued by the Performance & Aerodynamic Department. Engine Division Filton Bristol. Drawn by EAW. 24.5' diameter Canberra jet pipe; 22.6' nominal diameter nozzle. Gross jet thrust. TED.20049
-
Held by (Who holds the record)
- Coventry Archives & Research Centre
-
Language (The language of the record)
- English
-
Physical description (The amount and form of the record)
- 1 Item
-
Record URL
- https://beta.nationalarchives.gov.uk/catalogue/id/427cfb40-e54b-4278-bbd7-78fc9a672381/
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: PA1716/5/11/2/155
Bristol Aeroplane Co Ltd. Stress Department: Olympus 104 jet pipe characteristics