Frequency Characteristic Analysis of Liquid Rocket Propulsion System with Redundant Design
1.School of Mechanical Engineering,Tianjin University,Tianjin 300072,China;2.Beijing Institute of Astronautical Systems Engineering,Beijing 100076,China
WANG Tao1, RONG Yi2, HU Jiu-hui2, TANG Ye1, DING Qian1. Frequency Characteristic Analysis of Liquid Rocket Propulsion System with Redundant Design[J]. Journal of Propulsion Technology, 2021, 42(7): 1466-1475.
[1] Smith G, Philips A. Analysis of Parallel Burn, No-Crossfeed TSTO RLV Architectures and Comparison to Parallel Burn with Crossfeed and Series Burn Architectures[R]. AIAA 2003-5244.
[2] Souchier A, Pasquier J. Ariane 4 Liquid Boosters and First Stage Propulsion System[C]. Washington: 19th Joint Propulsion Conference, 1983.
[3] Martin J. Two-Stage Earth-to-Orbit Vehicles with Series and Parallel Burn[C]. Alabama: 22nd Joint Propulsion Conference, 1986.
[4] 马方超, 李德权, 吴 姮, 等. 液体火箭推进剂交叉输送系统试验研究[J]. 载人航天, 2017, 23(3): 358-364.
[5] 汤 波, 胡久辉, 邵业涛, 等. 液体运载火箭交叉输送总体参数研究[J]. 导弹与航天运载技术, 2017, (3): 22-27.
[6] Rubin S. Longitudinal Instability of Liquid Rockets Due to Propulsion Feedback(POGO)[J]. Journal of Spacecraft and Rockets, 1966, 3(8): 1188-1195.
[7] Tang Y, Li M, Wang L, et al. Modeling and Stability Analysis of Pogo Vibration in Liquid-Propellant Rockets with a Two-Propellant System[J]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2017, 60(2): 77-84.
[8] Zhao Z H, Ren G X, Yu Z W, et al. Parameter Study on POGO Stability of Liquid Rockets[J]. Journal of Spacecraft and Rockets, 2011, 48(3): 537-541.
[9] 谭述君, 王庆伟, 吴志刚. 临界阻尼比法在POGO振动稳定性分析中的适用性[J]. 宇航学报, 2015, 36(3): 284-291.
[10] 刘 涛, 刘锦凡, 唐国安. 液体火箭POGO振动分析的矢量拟合法[J]. 振动与冲击, 2019, 38(19): 26-30.
[11] Hao Y, Tang G A, Xu D Y. Finite-Element Modeling and Frequency-Domain Analysis of Liquid-Propulsion Launch Vehicle[J]. AIAA Journal, 2015, 53(11): 3297-3304.
[12] 唐 冶, 方 勃, 李明明, 等. 液体火箭推进系统频率特性的灵敏度分析[J]. 宇航学报, 2014, 35(8): 878-883.
[13] 唐 冶, 方 勃, 张业伟, 等. 推进系统参数变化对液体火箭纵向振动响应的影响分析[J]. 振动与冲击, 2015, 34(12): 189-194.
[14] 严 海, 方 勃, 黄文虎. 液体火箭的POGO振动研究与参数分析[J]. 导弹与航天运载技术, 2009(6): 35-40.
[15] 刘锦凡, 孙 丹, 陈雪巍, 等. 蓄压器膜盒机械刚度对液体火箭POGO振动影响研究[J]. 振动与冲击, 2016, 35(19): 168-171.
[16] 万屹仑, 付欣毓, 张黎辉, 等. 注气式蓄压器系统工作特性仿真分析[J]. 火箭推进, 2018, 44(3): 37-42.
[17] Oppenheinm B W, Rubin S. Advanced POGO Stability Analysis for Liquid Rockets[J]. Journal of Spacecraft and Rockets, 1993, 30(3): 360-373. .
[18] Wang Q W, Tan S J, Wu Z G, et al. Improved Modelling Method of POGO Analysis and Simulation for Liquid Rockets[J]. Acta Astronautica, 2015, 107: 262-273.
[19] Tan S, Wang Q, Wu Z, et al. A Method for Deriving a Non-Singular State-Space Formulation Based on Rubin's Model for Pogo Analysis[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(8): 2717-2730.