Cart

Shopping Cart

Copyright Policy

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
  • Prepare new works derived from the original (for example, a novel adapted into a play, or a translation, or a musical arrangement)
  • Publicly perform or display the work

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

Available coupons (Click to apply).

Cart totals

Subtotal $200.00
Tax $0.00
Total $200.00
Proceed to checkout