Results
This specification covers a silicone (PVMQ) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
This specification covers a high temperature, compression set and fluid resistant fluorocarbon (FKM) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes for aeronautical and aerospace applications.
This specification covers a polishing compound for aircraft metals in the form of a liquid or paste.
This specification covers a chloroprene (CR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
This specification covers an ethylene propylene (EPM) rubber in the form of sheet, strip, tubing, molded shapes, and extrusions.
This specification covers four classes of tungsten heavy metal in the form of sintered and annealed shapes.
This specification covers a low-alloy steel in the form of investment castings.
This specification covers an iron-nickel-cobalt alloy in the form of bars and forgings.
This specification covers a corrosion and heat resistant iron alloy sintered wire mesh in the form of sheet and strip.
This specification covers the requirements for a manganese phosphate coating on ferrous alloys.
Data are related to the dimensional changes with respect to room temperature and provide accuracy sufficient for use with most aerospace systems. Two basic methods of solution are presented with examples for steady state conditions involving uniform and non-uniform temperature distributions. The answers to the example problems are carried to the fifth place for a comparison of the results between Methods I and II.
This specification covers a corrosion and moderate heat resistant steel in the form of sand castings.
This specification covers a coating consisting of finely-powdered graphite in a heat-resistant inorganic binder.
This specification covers one type of copper in the form of sheet, strip, and plate.
This specification covers an aluminum alloy in the form of honeycomb core in a non-hexagonal, flexible cell configuration, the core being treated for increased corrosion resistance and furnished only in the expanded form.
This specification covers a magnesium alloy in the form of plate.
This specification covers bearings of a leaded bronze cast on one or both faces of a steel backing.
This specification covers one strength and one weave of mercerized cotton cloth known as "airplane cloth."
This specification covers an aluminum alloy in the form of hand forgings up to 8 inches, incl (203 mm, incl) in nominal thickness, and rolled rings up to 3.5 inches, incl (89 mm, incl) in nominal thickness (see 8.5).
This specification covers an iron-nickel alloy in the form of strip.
This specification covers one type of aluminum bronze in the form of bars, rods, forgings, and forging stock.
SAE J1333 applies to hydraulic cylinders which are components of self-propelled work machines defined in SAE J1116.
This specification covers the design requirements and test procedures for separable beam seal fittings which includes end fittings (see 2.3.4), fitting bodies (see 2.3.7), and boss fittings (see 2.3.2) for use in aerospace fluid systems. Design requirements are for class 3000 in corrosion resistant steel (15-5 PH, 17-4 PH CRES) only and for class 4000 in titanium alloy (Ti) and corrosion and heat-resistant steel (nickel alloy 718 CRES) only. Definition of fittings and related terms are defined in 2.3.
This specification covers polytetrafluoroethylene resin in the form of extruded rods, tubes, and shapes.
This specification covers the requirements for electrodeposited and diffused lead and indium plate.
This specification covers the requirements for electrodeposited low-stressed nickel.
This specification covers bearings of a tin alloy cast on one or both faces of a steel or bronze backing.
Items per page:
50
1 – 50 of 214147