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× 22. Preliminary Design Equations for Aircraft Weight Estimation 22. Preliminary Design Equations for Aircraft Weight Estimation $20.00
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× 846. Use of Mass Properties Data to Assess Engine Performance 846. Use of Mass Properties Data to Assess Engine Performance $20.00
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× 835. Loadability of 'Concorde' 835. Loadability of 'Concorde' $20.00
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× 842. A Merit Factor Suitable for Evaluation of a Variety of Aircraft Types and Missions 842. A Merit Factor Suitable for Evaluation of a Variety of Aircraft Types and Missions $20.00
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Subtotal $80.00
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Total $80.00