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<p>F1 through Leasat F5) were alternatively named Syncom IV-1 to Syncom IV-5, all using Hughes' HS-381 platform of satellite. These satellites were considerably larger than Syncoms 1 to 3, weighing 1.3 <a href="page.php?w=tonne">tonne</a>s each (over 7 tonnes with launch fuel). At , the satellites were the first to be designed for launch from the <a href="page.php?w=Space_Shuttle">Space Shuttle</a> payload bay, and were deployed like a <a href="page.php?w=Frisbee">Frisbee</a>. The satellites are 30&nbsp;rpm <a href="page.php?w=Spin-stabilized_satellite">spin-stabilized</a></p><p>
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