FIELD: rocket engineering. SUBSTANCE: leading shaped charge 1 is installed in fairing 3 on base 5. Internal contact 4 in front part 6 is cone-shaped or ogival, rear part 7 is cylindrical. The ratio of parts 6 and 7 is 1:(1.5 to 2.5). Reinforced plastic flange 8 is formed on the end of internal contact 4. Internal contact 4 is attached to base 5 by screws 9. EFFECT: improved design. 1 dwg
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Authors
Dates
1997-01-27—Published
1994-05-31—Filed