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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
× 3340. Design of an Engine Inertia Measuring Device 3340. Design of an Engine Inertia Measuring Device $20.00
$20.00
× 3320. Static Balancing a Device with Two or More Degrees of Freedom - (The Key to Obtaining High Performance on Gimbled Missile 3320. Static Balancing a Device with Two or More Degrees of Freedom - (The Key to Obtaining High Performance on Gimbled Missile $20.00
$20.00
× 3310. SumMassProps - An Excel VBA Solution for Summing Mass Properties 3310. SumMassProps - An Excel VBA Solution for Summing Mass Properties $20.00
$20.00
× 3322. Weight and Balance Considerations for Flight Test Aircraft On 3322. Weight and Balance Considerations for Flight Test Aircraft On $20.00
$20.00
× 3326. Evolution of a Blended Lifting Body for the Orbital Space Plane 3326. Evolution of a Blended Lifting Body for the Orbital Space Plane $20.00
$20.00
× 3327. Mass Properties In VTOL UAV Conceptual Design Software, Part 1: Overview and Beneral Algorithims 3327. Mass Properties In VTOL UAV Conceptual Design Software, Part 1: Overview and Beneral Algorithims $20.00
$20.00
× 3330. Weight Optimization Of Filament-Wound Pressure Vessels 3330. Weight Optimization Of Filament-Wound Pressure Vessels $20.00
$20.00
× 3316. New High Strength Glass Bubbles Survive Injection Molding Conditions 3316. New High Strength Glass Bubbles Survive Injection Molding Conditions $20.00
$20.00

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Subtotal $160.00
Tax $0.00
Total $160.00
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