RT Journal Article
ID 7f4a7e1d06755be1
A1 Pang, Wei Qiang
A1 De Luca, Luigi T. 
A1 Xu, Hui Xiang 
A1 Fan, Xue Zhong
A1 Li, Yong Hong 
A1 Xie, Wu Xi 
A1 Li, Yang 
T1 EFFECTS OF CL-20 ON THE PROPERTIES OF GLYCIDYL AZIDE POLYMER (GAP) SOLID ROCKET PROPELLANT
JF International Journal of Energetic Materials and Chemical Propulsion
JO IJEMCP
YR 2016
FD 2016-02-02
VO 15
IS 1
SP 49
OP 64
K1 solid propellant
K1 GAP
K1 CL-20
K1 hazardous properties
K1 combustion characteristics
AB The microstructures and granularity distributions of HMX and CL-20 particles were analyzed. Three industrial and research-type GAP-based solid propellants containing CL-20 particles, featuring the same nominal composition, were prepared and experimentally tested. The effects of CL-20 particles on the rheological properties, energetic properties, and the hazardous properties of GAP-based solid propellants were investigated. The properties mentioned above were also compared to those propellants
containing HMX. Also, the strand burning rate and the associated combustion properties of propellants were determined. It turned out that the GAP-based propellants containing CL-20 particles can be prepared and cast safely. GAP-based propellants containing CL-20 particles are more sensitive to impact and friction compared to propellants with HMX. However, the addition of CL-20 particles to the propellant formulation can increase the burning rate and affect the combustion behavior, when compared to the reference propellant.
PB Begell House
LK https://www.dl.begellhouse.com/journals/17bbb47e377ce023,5dd309a20470ca0d,7f4a7e1d06755be1.html