TY - GEN
T1 - The analysis on the rising section of experimental pressure in variable thrust pintle solid rocket motor
AU - Wei, Xiang Geng
AU - He, Guo Qiang
AU - Li, Jiang
AU - Zhou, Zhan Feng
PY - 2008
Y1 - 2008
N2 - The experimental system of non-coaxial pintle solid rocket motor was designed, and through this system, the experiments that validate variable thrust principle were carried out. A series of experiments were done, so as to find out how motor free volume, pintle movement state, cylinder sending pintle to some position by one time or not, equivalent throat structure, and propellant influence the response of pressure during the change of thrust. And by analyzing the results, it is concluded that the response time of propellant is the primary factor which effects the response of pressure.
AB - The experimental system of non-coaxial pintle solid rocket motor was designed, and through this system, the experiments that validate variable thrust principle were carried out. A series of experiments were done, so as to find out how motor free volume, pintle movement state, cylinder sending pintle to some position by one time or not, equivalent throat structure, and propellant influence the response of pressure during the change of thrust. And by analyzing the results, it is concluded that the response time of propellant is the primary factor which effects the response of pressure.
UR - http://www.scopus.com/inward/record.url?scp=77957831223&partnerID=8YFLogxK
M3 - 会议稿件
AN - SCOPUS:77957831223
SN - 9781563479434
T3 - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
BT - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
T2 - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Y2 - 21 July 2008 through 23 July 2008
ER -