| 摘要 |
A missile launcher comprising a forward support (501) for supporting a forward portion of a missile, and an aft support (505) for supporting an aft portion of the missile where the forward support (501) is arranged to swing clear of the aft portion of the missile during the initial period of its launching run where the forward support comprises a roll member (501) being in the shape of a segment of a circle and pivoted at the circle centre, where the perimeter of said member (501) is arranged to make frictional contact to the missile fuselage in order to confer mechanical energy to the roll member (501) to make said member to swing clear of the aft portion of the missile during the initial period of said missiles launching run.
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