FORFARANDE FOR UPPSKJUTNING AV SATELLITER OCH SATELLIT FOR SADANT FORFARANDE

摘要

The carrier rocket has a primary adapter component (2) for retention of the first satellite (3) during launching using a first fixture (8) releasable on command from the ground control. The free inner chamber (5) in the adapter component (2) has an opening (6) in the rocket direction of travel. The second satellite (7) which is smaller than the first (3) is placed for launching purposes in the free inner chamber (5) and points forwards.