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Fins vs Canards
Canard control - Good lift/latax control for moderate angles of attack. - Shed vortices can interfere with tail to generate roll moment. - Tendency to stall at high angle of attack-alleviated by fixed front canard.
Fin/tail control - Efficient packaging of subsystems. - Low hinge moment/acutator torque because of relatively low angle of attack. - Low induced roll moment (shed vortices are behind and do not interfere with other components). - Good efficiency at high angles of attack. - Poor lift/latax control for statically stable airframes because of low angle of attack. - Sometimes used with guidance vanes in rocket plume.
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Calculating the thrust of the engine: When applying the above method to calculate the individual thrust loads on the various components it is assumed that the engine is static.
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