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BSI
BS 6332-4:1983
Anulada
2008-03-31
Thermal performance of domestic gas appliances. Specification for
thermal performance of independent convector heaters
BSI
BS EN 4315:2007
En Vigor
2008-03-31
Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15).
Solution treated and precipitation treated, bar and section a or D ≤ 100
mm, Rm ≤ 900 MPaAerospace series. Heat resisting alloy FE-PA2601
(X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and
section a or D ≤ 100 mm, Rm ≤ 900 MPaAerospace series. Heat resisting
alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation
treated, bar and section a or D ≤ 100 mm, Rm ≤ 900 MPa
BSI
BS EN 4317:2007
En Vigor
2008-03-31
Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non
heat treated, forging stock a or D ≤ 200 mmAerospace series. Heat
resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non heat treated, forging
stock a or D ≤ 200 mmAerospace series. Heat resisting alloy FE-PA2601
(X6NiCrTiMoV26-15). Non heat treated, forging stock a or D ≤ 200 mm
BSI
BS EN 4318:2007
En Vigor
2008-03-31
Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15).
Solution treated and precipitation treated, bar and section De ≤ 100 mm,
Rm ≤ 960 MPaAerospace series. Heat resisting alloy FE-PA2601
(X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and
section De ≤ 100 mm, Rm ≤ 960 MPaAerospace series. Heat resisting alloy
FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation
treated, bar and section De ≤ 100 mm, Rm ≤ 960 MPa
BSI
BS EN 1266:2002
En Vigor
2008-02-29
Independent gas-fired convection heaters incorporating a fan to assist
transportation of combustion air and/or flue gases
BSI
BS EN ISO 5999:2004
Anulada
2008-02-29
Polymeric materials, cellular flexible. Polyurethane foam for
load-bearing applications excluding carpet underlay. Specification
BSI
BS EN ISO 1798:2000
Anulada
2008-02-29
Flexible cellular polymeric materials. Determination of tensile strength
and elongation at break
BSI
BS EN 3646-002:2007
En Vigor
2008-02-29
Aerospace series. Connectors, electrical, circular, bayonet coupling,
operating temperature 175°C or 200°C continuous. Specification of
performance and contact arrangements
