File
Bristol Aeroplane Company Limited. Stress Office. Engine Stress investigation: Olympus...
Catalogue reference: PA1716/5/11/2/337
What’s it about?
This record is a file about the Bristol Aeroplane Company Limited. Stress Office. Engine Stress investigation: Olympus... dating from 23 October 1953.
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)
- PA1716/5/11/2/337
-
Title (The name of the record)
- Bristol Aeroplane Company Limited. Stress Office. Engine Stress investigation: Olympus Mk.IV LP Compressor rotor blade tip clearances
-
Date (When the record was created)
- 23 October 1953
-
Description (What the record is about)
-
Ref: 4366/2. Performance calculations rederred to: 4366/2 & 4356/2. Contents: Page 1 Summary. Pages 2-3 calculations
-
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/c02778d8-2f61-4eb0-8df3-5459a2ac5f4f/
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: PA1716/5/11/2/337
Bristol Aeroplane Company Limited. Stress Office. Engine Stress investigation: Olympus Mk.IV LP Compressor rotor blade tip clearances