The off-set exhausts cause the missile to spin during flight with guidance control provided by two pop-out control surfaces at the rear of the missile (four additional surfaces help stabilise the missile during flight).
Guidance control is provided by two pop-out control surfaces at the rear of the missile (four additional surfaces help stabilise the missile during flight). The off-set exhausts cause the missile to spin during flight.
The off-set exhausts cause the missile to spin during flight. Guidance control is provided by two pop-out control surfaces at the rear of the missile (four additional surfaces help stabilise the missile during flight).
The off-set exhausts cause the missile to spin during flight. Guidance control is provided by two pop-out control surfaces at the rear of the missile (four additional surfaces help stabilise the missile during flight).