International Journal of Aerospace Engineering / 2015 / Article / Fig 10

Research Article

Firing Control Optimization of Impulse Thrusters for Trajectory Correction Projectiles

Figure 10

The impact of parameters of thrusters on CEP and flight stability of rockets.
(a) CEP versus number of thrusters and individual thruster impulse
(b) CEP versus total impulse of thrusters and individual thruster impulse
(c) Maximal total attack angle versus individual thruster impulse and minimum firing interval

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