Burning rate characterization of GAP/HMX energetic composite materials

Propellants, Explosives, Pyrotechnics

Volumn 25, Issue 4, 2000, Pages 168-171

  Kubota, Naminosuke ^a   Aoki, Ichiro ^b  

^a MITSUBISHI ELECTRIC CORPORATION   (Japan)

^b Hosoya Kako Co Ltd   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

ADDITION REACTIONS; AMINES; COMBUSTION; COMPOSITION EFFECTS; HEAT FLUX; PARTICLES (PARTICULATE MATTER); PHASE COMPOSITION; PRESSURE EFFECTS; REINFORCED PLASTICS;

CYCLOTETRAMETHYLENE TETRANITRAMINE; POLYGLYCIDYL AZIDE;

EXPLOSIVES;

EID: 0034245134     PISSN: 07213115     EISSN: None     Source Type: Journal    
DOI: 10.1002/1521-4087(200009)25:4<168::AID-PREP168>3.0.CO;2-B     Document Type: Article

References (3)

1. N. Kubota, "Survey of Rocket Propellants and Their Combustion Characteristics," in: K. K. Kuo and M. Summerfield (eds), "Fundamentals of Solid-Propellant Combustion", Progress in Astronautics and Aeronautics, Vol. 90, AIAA, Washington, DC, 1984, Chap. 1.
2. N. Kubota and T. Sonobe "Combustion Mechanism of Azide Polymer," Propellants, Explosives, Pyrotechnics 13, 172-177 (1988).
3. N. Kubota, "Combustion of Energetic Azide Polymers," J. Propul. Power 11(4), 677-682 (1995).