[1]夏长青,南宝江,王增辉,等.过载下丁羟推进剂压强耦合响应试验研究[J].固体火箭技术,2019,42(03):361-364.
 XIA Changqing,NAN Baojiang,WANG Zenghui,et al.Experimental research on pressure coupled response of HTPB propellant under overloading conditions[J].Journal of Solid Rocket Technology,2019,42(03):361-364.
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过载下丁羟推进剂压强耦合响应试验研究

参考文献/References:

[1]Coates R L.Application of T-burner to ballistic evaluation of new propellants[J].Journal of Spacecraft And Rockets,1966,3(12):1793-1796. [2]Horton M D,Coates R L.T-burners:Experiments compared with theory[J].Journal of Spacecraft and Rockets,1974,11(1):48-51.[3]Mihlfeith C M,Sayer L H.Novel high area ratio T-burner for characterizing metalized propellants[J].Journal of Spacecraft and Rockets,1974,11(8):574-578.[4]Beck W H,Jolleyt W H.Harmonic analysis of piston and pyrotechnic pulsers for T-burners[J].Journal of Spacecraft and Rockets,1988,4(3):283-285. [5]Jerry C Finlinson,Richard A Stalnaker,Fred S Blomshield.MHD T-burner combustion response test improvements[R].AIAA 99-2363.[6]Jerry C Finlinson,Richard Stalnaker,Fred S Blomshield.Ultra pure ammonium perchlorate T-burner pressure coupled response at 500,1000 and 1800 psi[C]//34th AIAA Joint Propulsion Conference,July,1998.[7]Jerry C Finlinson,Richard Stalnaker,Fred S Blomshield.HMX and RDX T-burner pressure coupled response from 200 to 1000 psi[C]//36th AIAA Aerospace Sciences Mtg,Jan,1998. [8]刘佩进,齐宗满,金秉宁,等.两种含铝复合推进剂压强耦合响应的实验对比[J].固体火箭技术,2013,36(1):83-88.LIU Peijin,QI Zongman,JIN Bingning,et al.Experiment comparison of pressure coupled response of the aluminized composite propellants[J].Journal of Solid Rocket Technology,2013,36(1):83-88.

更新日期/Last Update: 2019-07-11
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