n 12 Dec 1967 p 429-32. Performance of rocket or missile is very sensitive to nozzle efficiency, increase of 1% yielding in some cases 100% increase in payload; concept of plug-type nozzle, in which expansion fan rather than gradual increase of passage area is employed to expand combustion products to supersonic velocity. n 1 Jan 1968 p 33-6. Characteristics of truncated plug, annular and throttleable plug nozzles were investigated at Von Karman Institute for Fluid Dynamics and at Centro Nazionale di Ricerca sulla Tecnologia della Propulsione e dei Materiali Relativi, Milano, Italy; evaluation of performance and results of tests. (v 9 n 12 Dec 1967 p 429-32)
Experimental study on application of plug nozzles to solid-propellent rockets
Spaceflight
Spaceflight ; 10 , n 1
1967
4 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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