FIELD: application of coat on rocket engine manifold.
SUBSTANCE: coat is formed on at least one backing by feeding particles of metal powder through sprayer nozzle; size of particles is sufficient for excluding blowing-off by front of shock wave up to 50 mcm. Particles are passed through sprayer nozzle at rate sufficient for arising of plastic deformation of metal powder particles on at least one surface of backing. Carrier gas is fed to nozzle at flow rate of 0.028 to 1415.84 dm3/min.
EFFECT: avoidance of swelling after soldering at high temperature.
17 cl, 1 dwg
Authors
Dates
2005-12-27—Published
2003-10-20—Filed