Comparison between axially and radially burning charges shows that former charge can increase missile's range more than two-fold; functional relationships between factors involved are presented in graphs; main functions are discussed mathematically; basic difference between both charges is larger amount of propellant in axially burning rocket charge.
Advantages of higher combustion velocities in rocket propulsive charges
Vorteile hoeherer Abbrandgeschwindigkeiten bei Raketentreibsaetzen
Explosivstoffe ; 14 , n 4
1966
9 pages
Aufsatz (Zeitschrift)
Deutsch
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Propulsive potential of residual rocket motor heat
NTRS | 1968
|Propulsive Potential of Residual Rocket Motor Heat
NTIS | 1968
|Principles of rocket and jet propulsion and propulsive materials
Engineering Index Backfile | 1945
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