Patent ID: 7875838
Filing Date: 2011-01-25
Classification: F02K,F42B

Abstract:
1. A tubular distributor in a missile, comprising: (a) a right-angled hollow tubular first section, the right-angled hollow tubular first section comprising a first leg and a second leg; (b) a straight hollow tubular second section, an end of the first leg of the right-angled hollow tubular first section perpendicularly connected to a first end of the hollow tubular second section; (c) a straight hollow tubular third section, a first end of the hollow tubular third section perpendicularly connected to the first end of the straight hollow tubular second section, the hollow tubular third section being in line with the first leg of the right-angled hollow tubular first section, a hollow interior of the right-angled hollow tubular first section joined with a hollow interior of the straight hollow tubular third section, a hollow interior of the straight hollow tubular second section joined with a hollow interior of the straight hollow tubular third section; and (d) a close/open valve positioned within the straight hollow tubular third section, the close/open valve positioned between a gas generator and the straight hollow tubular second section.