TY - JOUR
T1 - HTPB推进剂"脱湿"性能表征及影响因素试验研究
AU - Zhang, Zhenguo
AU - Zhang, Hongliang
AU - Hou, Xiao
AU - Yan, Tao
AU - Gao, Jie
N1 - Publisher Copyright:
© 2020, Editorial Dept. of JSRT. All right reserved.
PY - 2020/6/1
Y1 - 2020/6/1
N2 - In order to study the dewetting performance of HTPB propellant, a device for testing propellant dewetting performance was developed based on the principle of gas dilatometer, and the test of the influence of formulation and strain rate on the dewetting performance of the propellant was carried out by using the device. The initial dewetting point, characteristic dewetting point and characteristic dewetting rate were used to characterize the dewetting performance of propellant. The test results show that the dewetting performance of propellant has obvious rate correlation, the higher the strain rate is, the smaller the initial dewetting point and characteristic dewetting point of propellant are, and the higher the characteristic dewetting rate is, but there is an upper limit on the internal dewetting rate of the propellant; the effect of AP content on the dewetting performance of HTPB propellant is dominant, and the higher AP content is, the smaller the initial dewetting point and characteristic dewetting point are and the higher the characteristic dewetting rate is. The established test method and dewetting performance characterization method are of important practical significance for structural integrity, mechanical property prediction and reliability evaluation of the grain.
AB - In order to study the dewetting performance of HTPB propellant, a device for testing propellant dewetting performance was developed based on the principle of gas dilatometer, and the test of the influence of formulation and strain rate on the dewetting performance of the propellant was carried out by using the device. The initial dewetting point, characteristic dewetting point and characteristic dewetting rate were used to characterize the dewetting performance of propellant. The test results show that the dewetting performance of propellant has obvious rate correlation, the higher the strain rate is, the smaller the initial dewetting point and characteristic dewetting point of propellant are, and the higher the characteristic dewetting rate is, but there is an upper limit on the internal dewetting rate of the propellant; the effect of AP content on the dewetting performance of HTPB propellant is dominant, and the higher AP content is, the smaller the initial dewetting point and characteristic dewetting point are and the higher the characteristic dewetting rate is. The established test method and dewetting performance characterization method are of important practical significance for structural integrity, mechanical property prediction and reliability evaluation of the grain.
KW - Characteristic dewetting rate
KW - Dewetting performance
KW - Dewetting point
KW - Gas dilatometer
KW - HTPB propellant
UR - http://www.scopus.com/inward/record.url?scp=85090632715&partnerID=8YFLogxK
U2 - 10.7673/j.issn.1006-2793.2020.03.001
DO - 10.7673/j.issn.1006-2793.2020.03.001
M3 - 文章
AN - SCOPUS:85090632715
SN - 1006-2793
VL - 43
SP - 265
EP - 270
JO - Guti Huojian Jishu/Journal of Solid Rocket Technology
JF - Guti Huojian Jishu/Journal of Solid Rocket Technology
IS - 3
ER -