Yes, i was asking if that type of attitude control can be achieved and if that configuration would give greater crossrange capability.
I wonder if an spacecraft with an attitude control system like this can have more control of the capsule in the reentry, giving more landing sites options and...
I understand that on Blunt or conical Bodies like Soyuz or Apollo the reentry attitude is achieved by carefully trimming of capsule centre of gravity.
I was reading last night a document that states that better spacecraft control and cross range can be obtained by adding this capsules a flap...
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