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All SAWE books, technical papers, recommended practices, and handbooks which are published/distributed by SAWE are SAWE copyrighted property. Anyone who does any of the following without authorization from SAWE infringes on that copyright:

  • Reproduce the work by making copies of it
  • Distribute copies of the work to the public by sale, donation, rental, or lending
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For Corporate Partners and Company Members with an active membership, documents associated with membership benefits are made accessible on SAWE cloud services.  The copying/distribution restrictions highlighted above still apply. Please contact the SAWE Executive Director for questions or concerns.

Remove item Thumbnail image Product Price Quantity Subtotal
× 10. Calculation of Landing Gear and Hydraulic System Weights 10. Calculation of Landing Gear and Hydraulic System Weights $20.00
$20.00
× 985. The STAN(R)'S' Integral Weight and Balance System for the C-130 Aircraft 985. The STAN(R)'S' Integral Weight and Balance System for the C-130 Aircraft $20.00
$20.00
× 974. Weight Engineering - An Opinionnaire 974. Weight Engineering - An Opinionnaire $20.00
$20.00
× 982. A Computer-Aided Design Procedure to Approximate Aircraft Area Curve Shapes 982. A Computer-Aided Design Procedure to Approximate Aircraft Area Curve Shapes $20.00
$20.00
× 967. The Weight/Performance Interface - An Argument for Weight Control 967. The Weight/Performance Interface - An Argument for Weight Control $20.00
$20.00
× 30. The Effect of Center of Gravity on Performance 30. The Effect of Center of Gravity on Performance $20.00
$20.00
× 984. Weight Change - Where Does It Come From 984. Weight Change - Where Does It Come From $20.00
$20.00
× 27. The Significance of Weight Control 27. The Significance of Weight Control $20.00
$20.00
× 22. Preliminary Design Equations for Aircraft Weight Estimation 22. Preliminary Design Equations for Aircraft Weight Estimation $20.00
$20.00
× 971. Rocket Power, Redstone to Saturn V, Now Space Shuttle 20 Years of Development 971. Rocket Power, Redstone to Saturn V, Now Space Shuttle 20 Years of Development $20.00
$20.00
× 992. Boron Composites - Development and Application Status 992. Boron Composites - Development and Application Status $20.00
$20.00
× 983. Advanced Design Mass Property Estimates by Detail Weight Calculations (A Case for the Rhoving Mass Properties Engineer) 983. Advanced Design Mass Property Estimates by Detail Weight Calculations (A Case for the Rhoving Mass Properties Engineer) $20.00
$20.00
× 25. The Effect of Overload and Unbalance on Long Range Operation 25. The Effect of Overload and Unbalance on Long Range Operation $20.00
$20.00

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Subtotal $260.00
Tax $0.00
Total $260.00
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