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Provided that we have got two different missiles by name(A & B) but yet they have in common the guidance system as well as the engine say a turbofan; can they be called a single missile having two versions i.e air launched & land launched??
If not does this mean that though both have turbofans but thrust profiles/specific impulses are different for air & land launched missiles??
I do know that there will be some aerodynamic diffences but what about internal makeup??
If not does this mean that though both have turbofans but thrust profiles/specific impulses are different for air & land launched missiles??
I do know that there will be some aerodynamic diffences but what about internal makeup??