The Advanced Solid Propulsion Technologies Based on the Self-Propagating High-Temperature Synthesis Processes

Proceedings of the 2003 International Autumn Seminar on Propellants, Explosives and Pyrotechnics (2003 IASPEP) - Theory and Practice of Energetic Materials

Volumn 5, Issue , 2003, Pages 3-20

  Lukin, Alexander ^a  

^a Institute of Applied Mechanics   (Russian Federation)

Author keywords

Abnormal high burning rate; Compensators of the burning surface; Ignition transient period of operation; Propellant charge ignition delay time; Pyrotechnic ignition system; Self propagating high temperature synthesis processes; Solid propulsion systems

Indexed keywords

BALLISTICS; COMBUSTION CHAMBERS; FLAMMABILITY; IGNITION; IMPACT RESISTANCE; METAL FOIL; MICROSTRUCTURE; MULTILAYERS; OPTIMIZATION; PROPULSION; ROCKETS; VIBRATIONS (MECHANICAL);

ABNORMAL HIGH BURNING RATE; COMPENSATORS OF THE BURNING SURFACES; IGNITION-TRANSIENT PERIOD OF OPERATION; NANO-DIMENSIONAL MULTILAYERED FOIL; PROPELLANT CHARGE IGNITION DELAY TIME; PYROTECHNIC IGNITION SYSTEM; SELF-PROPAGATING HIGH-TEMPERATURE SYNTHESIS PROCESSES; SOLID PROPULSION SYSTEMS;

SOLID PROPELLANTS;

EID: 2342652955     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (20)

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