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× 1913. Aluminum Lithium for the F/A-18, Hornet 2000 1913. Aluminum Lithium for the F/A-18, Hornet 2000 $20.00
$20.00
× 1900. Launch Vehicle Synthesis and a Computer Modeling Approach 1900. Launch Vehicle Synthesis and a Computer Modeling Approach $20.00
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× 1901. Derivation - A Fuselage Weight Estimating Relationship 1901. Derivation - A Fuselage Weight Estimating Relationship $20.00
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× 782. Heavy Lift VTOL - Effect of Weight and Size on Productivity 782. Heavy Lift VTOL - Effect of Weight and Size on Productivity $20.00
$20.00

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Subtotal $80.00
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Total $80.00