| Citation: | ZHANG Bin, MAO Gen-wang, HU Song-qi, CHEN Mao-lin. Investigation on plume interference effect of solid propellant micro-thruster[J]. Journal of Aerospace Power, 2011, 26(9): 2027-2031. |
| [1] |
Rossi C,Orieux S,Larangot B,et al.Design,fabrication and modeling of solid propellant microrocket-application to micropropulsion[J].Sensors and Actuators A,2002,99(1-2):125-133.
|
| [2] |
Zhang K L,Chou S K,Ang S S,et al.A MEMS-based solid propellant microthruster with Au/Ti igniter[J].Sensors and Actuators A,2005,122(1):113-123.
|
| [3] |
Chaalane A,Rossi C,Estève D.The formulation and testing of new solid propellant mixture(DB+x%BP) for a new MEMS-based microthruster[J].Sensors and Actuators A,2007,138(1):161-166.
|
| [4] |
ZHOU Haiqing,ZHANG Gaofei,YOU Zheng.Design and numerical analysis on a solid micro-thruster[J].Journal of Propulsion Technology,2007,28(3):230-234.(in Chinese)
|
| [5] |
Zhang K L,Chou S K,Ang S S.Development of a solid propellant microthruster with chamber and nozzle etched on a wafer surface[J].Journal of Micromechanics and Microengineering,2004,14(6):785-792.
|
| [6] |
Rossi C,Rouhani M D,Estève D.Prediction of the performance of a Si-micromachined microthruster by computing the subsonic gas flow inside the thruster[J].Sensors and Actuators A,2000,87(1-2):96-104.
|
| [7] |
HUANG Lin,NIE Wansheng,CHEN Weifang. Studying of multi-plume interference effects for attitude-control thruster with DSMC method[J].ACTA Aerodynamica Sinica, 2003,21(1):104-108.(in Chinese)
|
| [8] |
Bird G A.Molecular gas dynamics and the direct simulation of gas flows[M].Oxford:Clarendon Press,1994.
|
| [9] |
Gallis M A,Torczynski J R,Rader D J.An approach for simulating the transport of spherical particles in a rarefied gas flow via the direct simulation Monte Carlo method[J].Physics of Fluids,2001,13(11):3482-3492.
|
| [10] |
Gimelshein S F,Alexeenko A A,Wadsworth D C,et al.The influent of particulates on thruster plume/shock layer interaction at high altitudes .AIAA-2005-766,2005.
|
| [11] |
Burt J M,Boyd I D.Development of a two-way coupled model for two phase rarefied flows .AIAA-2004-1351,2004.
|
| [12] |
Burt J M.Monte Carlo simulation of solid rocket exhaust plumes at high altitude .Ann Arbor:University of Michigan,2006.
|