Launching tube for missiles

Ordnance – Rocket launching – Having tubular guide means

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F41F 3048

Patent

active

046466185

ABSTRACT:
A launching tube with an internal guide surface for effecting controlled spin for missiles, such as rockets, wherein the launching tube is provided on the inside with helically extending grooves and/or ridges contacting guide cams or the like of the missiles for guiding therealong. This launching tube is extruded, and sized, from a molding composition containing fiber-reinforced thermoplastic synthetic resin, to have integrally formed, slightly helically extending grooves and/or ridges.

REFERENCES:
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patent: 3228298 (1966-01-01), Grandy
patent: 3298279 (1967-01-01), Barnet et al.
patent: 3548707 (1970-12-01), Hughes
patent: 3673916 (1972-07-01), Wittholz
patent: 3857320 (1974-12-01), Conard
patent: 4095508 (1978-06-01), Lienau
patent: 4137819 (1979-02-01), Loomis
patent: 4227438 (1980-10-01), Precoul
`H. F. Mark, et al: Encyclopedia of Polymer Science and Technology`, Part 12, "Reinforced Plastics to Starch", 1974, Interscience, N.Y., USA, pp. 31-40.
`H. F. Mark, et al: Encyc. of Polymer Science & Technology`, Part 8, "Keratin to Modacrylic Fibres", 1974, Interscience, N.Y., USA, pp. 785-787.

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