| Citation: | ZENG Peng, TIAN Hui, LI Xin-tian, CAI Guo-biao. Orthogonal optimal design of solid fuel formulation for H2O2/HTPB hybrid rocket motor[J]. Journal of Aerospace Power, 2013, 28(5): 1180-1186.
|
| [1] |
Zilliac G.Hybrid rocket propulsion:past,present,and future[R].NASA Ames Research Center,2010.
|
| [2] |
Karabeyoglu A.Hybrid rocket propulsion for future space launch[R].Palo Alto,US:Space Propulsion Group Inc,2008.
|
| [3] |
杨玉新,胡春波,何国强,等.固液混合火箭发动机中的关键技术及其发展[J].宇航学报,2008,29(5):1616-1621. YANG Yuxin,HU Chunbo,HE Guoqiang,et al.Key technique of hybrid rocket motor and its development[J].Journal of Astronautics,2008,29(5):1616-1621.(in Chinese)
|
| [4] |
Davydenko N A,Gollender R G,Gubertov A M,et al.Hybrid rocket engines:the benefits and prospects[J].Aerospace Science And Technology,2007,11(1):55-60.
|
| [5] |
胡建新,夏智勋,张钢锤.固液火箭发动机在空间发射上的应用前景[J].导弹与航天运载技术,2002(3):18-22. HU Jianxin,XIA Zhixun,ZHANG Gangchui.The opportunity for hybrid rocket motor in commercial space applications[J].Missiles and Space Vehicles,2002(3):18-22.(in Chinese)
|
| [6] |
单建胜,雷宁.固液混合发动机的研制及其应用[J].固体火箭技术,1997,20(3):13-20. SHAN Jiansheng,LEI Ning.The development and applications of solid-liquid hybrid rocket motors[J].Journal of Solid Rocket Technology,1997,20(3):13-20.(in Chinese)
|
| [7] |
田辉,蔡国飙,孙再庸.N2O/HTPB固液火箭发动机喷管两相流计算[J].航空动力学报,2008,23(6):1146-4450. TIAN Hui,CAI Guobiao,SUN Zaiyong.Computation of nozzle two-phase flow in a N2O/HTPB hybrid rocket motor[J].Journal of Aerospace Power,2008,23(6):1146-4450.(in Chinese)
|
| [8] |
田辉,蔡国飙,王慧玉,等.固液混合火箭发动机喷管流动计算[J].航空动力学报,2005,20(1):142-146. TIAN Hui,CAI Guobiao,WANG Huiyu,et al.Nozzle flow computation of classical hybrid rocket motors[J].Journal of Aerospace Power,2005,20(1):142-146.(in Chinese)
|
| [9] |
Chiaverini M J,Kuo K K,Peretz A,et al.Regression-rate and heat-transfer correlations for hybrid rocket combustion[J].Journal of Propulsion and Power,2001,17(1):99-110.
|
| [10] |
Chiaverini M J,Serin N,Johnson D K,et al.Regression rate behavior of hybrid rocket solid fuels[J].Journal of Propulsion and Power,2000,16(1):125-132.
|
| [11] |
Chiaverini M J,Harting G C,Kuo K K.Pyrolysis behavior of hybrid-rocket solid fuels under rapid heating conditions[J].Journal of Propulsion and Power,1999,15(6):888-895.
|
| [12] |
George P,Krishnan S,Varkey P M,et al.Fuel regression rate in hydroxyl-terminated-polybutadiene/gaseous-oxygen hybrid rocket motors[J].Journal of Propulsion and Power,2001,17(1):35-42.
|
| [13] |
Frederick R A,Jr Whitehead J J,Knox L R,et al.Regression rates study of mixed hybrid propellants[J].Journal of Propulsion and Power,2007,23(1):175-180.
|
| [14] |
Peretz A,Einav O,Hashmonay B A,et al.Development of a laboratory-scale system for hybrid rocket motor testing[J].Journal of Propulsion and Power,2011,27(1):190-196.
|
| [15] |
Risha G A,Ulas A,Boyer E,et al.Combustion of HTPB-based solid fuels containing nano-sized energetic powder in a hybrid rocket motor[R].AIAA 2001-3535,2001.
|
| [16] |
Risha G A,Boyer E,Wehrman R B,et al.Performance comparison of HTPB-based solid fuels containing nano-sized energetic powder in a cylindrical hybrid rocket motor[R].AIAA 2002-3576,2002.
|
| [17] |
Risha G A,Evans B J,Boyer E,et al.Nano-sized aluminum and boron-based solid fuel characterization in a hybrid rocket engine[R].AIAA 2003-4593,2003.
|
| [18] |
Risha G A.Enhancement of hybrid rocket combustion performance using nano-sized energetic particles[D].Central County,US:The Pennsylvania State University,2003.
|
| [19] |
Evans B,Boyer E,Kuo K K.Hybrid rocket investigations at Penn State University's high pressure combustion laboratory overview and recent results[R].AIAA 2009-5349,2009.
|
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