File
Minutes of D.Eng.RD meeting held at Armstrong Siddeley Motors
Catalogue reference: PA1716/4/6/18
What’s it about?
This record is a file about the Minutes of D.Eng.RD meeting held at Armstrong Siddeley Motors dating from 11 June 1953.
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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)
- PA1716/4/6/18
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Title (The name of the record)
- Minutes of D.Eng.RD meeting held at Armstrong Siddeley Motors
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Date (When the record was created)
- 11 June 1953
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Description (What the record is about)
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Sapphire test position: Sa.7 fatigue failure of three 7th row compressor rotor blades in root serrations. Future programme. Sapphire 6 150-hour modification approval test ok. Reheat development. Sapphire 5 Attempted 25-hour special category test terminated after 5 hours due to severe compressor rotor blade tip foul. Thrust reversal. Sapphire Hastings: withdrawal of engines from aircraft. General development: (g) Request by DOR of a +10% thrust for emergency on fighter aircraft. Flying test beds: AST Lancastrian VM.733 (2 Sa.6 outboard engines); Gloster Meteor WA.820 (two Sa.2 engines); Canberra WD.933 (two Sa.3engines); Canberra (2nd aircraft) two Sa.6R engines. Prototype aircraft: Javelin WD.808 (two Sa.6) 2nd aircraft ; Javelin WD.827 (two Sa.6) rd aircraft; Handley Page HP.80 WB.771 (4 Sa.6) 1st aircraft; Handley Page 2nd aircraft awaiting delivery of engines due March/April 1953; Hawker Hunter WB.202 (Sa.6); English Electric P.1 (two Sa.5); Hawker Hunter (Sa.7). Adder: Disposal instructions for ASA.23. Viper test position: Requirement for two Viper engines (long life) for Provost aircraft provisioned to Armstrong Siddeley Motors. Double Mamba test position. Fairey flight engines for hot weather trials. Future development: 3-stage turbine. Aircraft: Fairey Gannet VR.546; Fairey Gannet (2nd aircraft) VR.557; Fairey Gannet (3rd aircraft) WE.488; Blackburn GR17/45 WB.797. Mamba test position: Armstrong Siddeley Motors.5 Armstrong Siddeley Motors.6. Additional engines for Dakota. SB.6 prototype flight engines. Lancaster SW.342; Dakota KJ.839; Balliol VL.935; SHort SB.6 (M.123.D) 1st aircraft Armstrong Siddeley Motors Mk.3 Sturgeon type engines ASZ.172 and ASZ.173 for initial flying. 2nd aircraft with Armstrong Siddeley Motors Mamba Mk.6 engines. 3rd aircraft with Armstrong Siddeley Motors Mamba Mk.6 engines. Python: Wyvern VW.868 provisioned for Armstrong Siddeley Motors. Rocket: Screamer rocket motor. Requirement for Viper engines and rocket motors for intercepter aircraft. Provision of aircraft for Screamer tests confirmed for delivery to Armstrong Siddeley Motors June 1953. APU operating on rocket propellants Appendix 1: Sapphire. Appendix 2: Python. Appendix 3: Mamba. Appendix 4: Double Mamba. Appendix 5: Adder. Appendix 6: Viper.
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Held by (Who holds the record)
- Coventry Archives & Research Centre
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Former department reference (Former identifier given by the originating creator)
- Derd/1953
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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/7144e350-ff27-46d6-aa49-95a0b61ca23f/
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: PA1716/4
Bitteswell Flight Testing (A History)
Within the sub-sub-fonds: PA1716/4/6
Minutes of D.Eng.RD meetings held at Armstrong Siddeley Motors
You are currently looking at the file: PA1716/4/6/18
Minutes of D.Eng.RD meeting held at Armstrong Siddeley Motors