Thrust Control Features for Aerodynamic Throat for
Solid Rocket Motor
（School of Aerospace Engineering，Beijing Institute of Technology，Beijing 100081，China）,（School of Aerospace Engineering，Beijing Institute of Technology，Beijing 100081，China）,（School of Aerospace Engineering，Beijing Institute of Technology，Beijing 100081，China） and （School of Aerospace Engineering，Beijing Institute of Technology，Beijing 100081，China）
XIE Kan,LI Bo,GUO Chang-chao,WANG Ding-fei. Thrust Control Features for Aerodynamic Throat for
Solid Rocket Motor[J]. Journal of Propulsion Technology, 2015, 36(2): 194-199.
[1] 张淑惠, 湖波, 孟雅桃. 推力可控固体火箭发动机应用及发展[J]. 固体火箭技术, 2002, 25(4): 12-15.
[2] Jcffrcy A Cdtt, Daniel N Hlillcr. A Static Investigation of Rxed-Geometry Nozzles Using Fluidic Injection for Throat Area Contros[R]. AIAA 95-2604.
[3] Y Damiel N Miller, Patrick J Yagle, Jeffrey W Hamstra.Fluidic Throat Skewing for Thrust Vectoring in Fixed-Geometry Nozzles[R]. AIAA 99-0365.
[4] Martin A I. The Aerodynamic Variable Nozzle[J]. Journal of Aeronautical Sciences, 1951, 24(5): 357.
[5] Dan Baruzzini, Neal Domel, Daniel N Miller et al. Pulsed Injection Flow Control for Throttling in Supersonic Nozzles-A Computational Fluid Dynamics Design Study[R]. AIAA 2007-4215.
[6] John N, Victoria G. Controllable Solid Propulsion for Launch Vehicle and Spacecraft Application[R]. AIAA 2006-0468.
[7] Mason M S, Crowther W J. Fluidic Thrust Vectoring for Low Observable Air Vechicles[R]. AIAA 2004-2210.
