Role of research rocket and types of vehicle for environmental measurement; design of ballistic rockets; main criteria used in choosing design for Black Knight; development of complete system; first stage has liquid propellant rocket motor using HTP and kerosene which have specific impulse at sea level of 240 sec at 500 lb/sq in.; control and guidance system; second stage; instrumentation; ground facilities; rocket firings.
Ballistic research rockets with particular reference to Black Knight
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 65 , n 603
1961
19 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Impact points of ballistic rockets
Engineering Index Backfile | 1957
|Discussion of the Control Systems of Ballistic Rockets
NTIS | 1970
|Method for calculating impact points of ballistic rockets
Engineering Index Backfile | 1957
|