This chapter contains sections titled:
Combustion Phenomena in a Rocket Motor
Propellant Combustion in a Rocket Motor
Stability Criteria of Rocket Motor
Temperature Sensitivity of Pressure in a Rocket Motor
Ignition Transient
Convective Ignition
Radiative Ignition
Ignition Transient in Rocket Motor
Erosive Burning
Erosive Burning in a Rocket Motor
Erosive Burning Mechanism
Wired‐Propellant Burning
Combustion Instability
T*‐Combustion Instability
L*‐Combustion Instability
Acoustic Combustion Instability
Ducted Rocket Engine
Propulsion of a Ducted Rocket
Principle of the Variable Flow Ducted Rocket
Energetics of Gas‐Generating Propellants
Combustion in a Rocket Motor
Propellants and Explosives ; 205-231
2001-12-21
27 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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