Investigation on Performance of Small-Thrust Bi-Propellant Thruster for Attitude Control
School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;Beijing Institute of Control Engineering, Beijing 100190, China;Beijing Institute of Control Engineering, Beijing 100190, China;Beijing Institute of Control Engineering, Beijing 100190, China;School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
[1] Schwende M A, Munding G, Schulte G.Bi-Propellant Thruster Family for Spacecraft Propulsion[R].AIAA 92-3860. [2] Wang X F, Chin J S, Lefebvre A H.Influence of Gas-Injector Geometry on Atomization Performance of Aerated Liquid Nozzles[J].International Journal of Turbo and Jet-Engines, 9,6(4):271-279. [3] Rossler T C, Lefebvre A H.Studies on Aerated-Liquid Atomization[J].International Journal of Turbo and Jet-Engines, 9,6(7):221-229. [4] Chen S K, Lefebvre A H, Roubuhler J.Influence of Ambient Air Pressure on Effervescent Atomization[J].AIAA Journal of Propulsion and Power, 3,9(5):10-15. [5] Schwende M A, Schulte G.Test Results for Second-Generation Low Thrust Bipropellant Engines[R].AIAA 93-686. [6] Gotzig U, Schulte G, Sowa A.New Generation 10N Bipropellant MMH/NTO Thruster with Double Seat Valve[R].AIAA 99-2594. [7] Schulte G, Horch A.Further Improvements and Qualification Status of Astriums 10N Bipropellant Thruster Family[R].AIAA 2003-4776. [8] Stechman R.Development and Qualification of a 2nd Generation 5 lbf (22N) Bipropellant Thruster[R].AIAA 89-2734. [9] Wood R S.Development Experience with 22N Bipropellant Thrusters Using Columbium and Rhenium Thrust Chambers[R].AIAA 92-3801. [10] Gousy R G, Kent S.Extended Pressure Range Performance of the Atlantic Research 22N Thruster[R].AIAA 93-2520.