It is shown how performance has improved during past decade and how they can provide controlled thrust to meet any missile requirement; thrust control for solid propellant engines and three methods which would be applicable, namely, jet vanes, inclined tubular extension, and sliding beveled extension or ungulus; control of thrust magnitude.
Future for solid propellant rockets
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 63 , n 580
1959
6 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
NTIS | 1967
|NTRS | 1964
|Engineering Index Backfile | 1955
|NTIS | 1968
|Machining for solid propellant rockets
Engineering Index Backfile | 1957
|