Piece
Accessions administration: AVIA 37
Catalogue reference: PRO 57/14552
Date: 2001 Jan 1 - 2003 Dec 31
Accessions administration: AVIA 37
Piece
Working Party on Thrust Efficiency of Aluminised Propellants: first progress report
Catalogue reference: AVIA 37/1234
What’s it about?
This record is about the Working Party on Thrust Efficiency of Aluminised Propellants: first progress report dating from 1960 in the series Ministry of Supply and Ministry of Aviation: Chemical Research and Development Department.... It is held at The National Archives, Kew.
Is it available online?
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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)
- AVIA 37/1234
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Date (When the record was created)
- 1960
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Description (What the record is about)
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Working Party on Thrust Efficiency of Aluminised Propellants: first progress report
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Held by (Who holds the record)
- The National Archives, Kew
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Former department reference (Former identifier given by the originating creator)
- ERDE 7/TN/60
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Legal status (A note as to whether the record being described is a Public Record or not)
- Public Record(s)
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Closure status (Whether the record is ‘open’ (available to the public) or ‘closed’ (not available due to a legal exemption))
- Open Document, Open Description
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Record URL
- https://beta.nationalarchives.gov.uk/catalogue/id/C635506/
How to order it
- View this record page in our current catalogue
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- Select an option and follow instructions
Series information
AVIA 37
Ministry of Supply and Ministry of Aviation: Chemical Research and Development Department...
See the series level description for more information about this record.
Catalogue hierarchy
Over 27 million records
This record is held at The National Archives, Kew
96,520 records
Within the department: AVIA
Records created or inherited by the Ministry of Aviation and successors, the Air...
1,457 records
Within the series: AVIA 37
Ministry of Supply and Ministry of Aviation: Chemical Research and Development Department...
You are currently looking at the piece: AVIA 37/1234
Working Party on Thrust Efficiency of Aluminised Propellants: first progress report
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