Development of Jet Vanes for Solid Propellant Missiles

620460

01/01/1962

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
Jet vanes as a means of guidance for missiles are reliable, low in cost, and produce less than 1% thrust loss. Jet vane metals or alloys must meet certain requirements, the primary one being a melting point above the missile's flame temperature. Alloys of tungsten and molybdenum appear to be the most promising. Comparing sintered and cast metals, castings for jet vanes are very satisfactory, and are preferable over the sintered material.
Meta TagsDetails
DOI
https://doi.org/10.4271/620460
Pages
9
Citation
Ahearn, R., "Development of Jet Vanes for Solid Propellant Missiles," SAE Technical Paper 620460, 1962, https://doi.org/10.4271/620460.
Additional Details
Publisher
Published
Jan 1, 1962
Product Code
620460
Content Type
Technical Paper
Language
English