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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
  • 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
× 32. Weight and It's Effect on the Operation and Performance of Commercial Aircraft 32. Weight and It's Effect on the Operation and Performance of Commercial Aircraft $20.00
$20.00
× 1703. Computer Generated 3-Dimensional Graphics and Mass Properties Application 1703. Computer Generated 3-Dimensional Graphics and Mass Properties Application $20.00
$20.00
× 1692. Comparison of Satellite Support Structure - Aluminum Versus Graphite Epoxy 1692. Comparison of Satellite Support Structure - Aluminum Versus Graphite Epoxy $20.00
$20.00
× 1721. The Variation of Gravity and Its Application to the Measurement of Weight 1721. The Variation of Gravity and Its Application to the Measurement of Weight $20.00
$20.00
× 1717. Gulfstream Corporate Aircraft Design Evolution Through the Model Gulfstream IV 1717. Gulfstream Corporate Aircraft Design Evolution Through the Model Gulfstream IV $20.00
$20.00
× 1734. NOTAR Helicopter - A New Approach to Helicopters 1734. NOTAR Helicopter - A New Approach to Helicopters $20.00
$20.00
× 1706. MASPROP - Computer Aided Mass Properties at Hughes Aircraft, Missile Systems Group 1706. MASPROP - Computer Aided Mass Properties at Hughes Aircraft, Missile Systems Group $20.00
$20.00
× 1742. An Operational Loading Analysis of the B-757-232 Aircraft 1742. An Operational Loading Analysis of the B-757-232 Aircraft $20.00
$20.00
× 1731. WISORD (Weight Interactive Synthesis and Optimization of Rotorcraft Design) 1731. WISORD (Weight Interactive Synthesis and Optimization of Rotorcraft Design) $20.00
$20.00
× 1722. Predicting Tilt of a Double Pendulum 1722. Predicting Tilt of a Double Pendulum $20.00
$20.00

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Subtotal $200.00
Tax $0.00
Total $200.00
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