Print Email Facebook Twitter Development tests on a gas valve for use on the R.A.E. 6in. shock tube at pressures up to 15,000 P.S.I. Title Development tests on a gas valve for use on the R.A.E. 6in. shock tube at pressures up to 15,000 P.S.I. Author Cox, S.G. Institution Royal Aircraft Establishment RAE Date 1962-10-31 Abstract This note describes a type of gas valve which was supplied for use on the R.A.E. 6 inch shock tube for use at pressures up to 15,000 p.s.i. and the development and acceptance tests that were carried out on it before it could be accepted as suitable for the required duty. To reference this document use: http://resolver.tudelft.nl/uuid:0c61a908-6205-4ee4-b79a-8cb431f58a78 Publisher Ministry of Aviation, Royal Aircraft Establishment, RAE Farnborough Access restriction Campus only Source RAE Technical Note No. Aero 2850 Part of collection Aerospace Engineering Reports Document type report Rights © 1962 Ministry of Aviation, Royal Aircraft Establishment Files PDF Tech Note Aero 2850.pdf 8.37 MB Close viewer /islandora/object/uuid:0c61a908-6205-4ee4-b79a-8cb431f58a78/datastream/OBJ/view