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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
× 179. The Structural Index - A Guide to Optimum Design 179. The Structural Index - A Guide to Optimum Design $20.00
$20.00
× 3435. Providing The Inertia Properties of Vehicles and Their Subsystems for Virtual Reality and Mechatronics Applications 3435. Providing The Inertia Properties of Vehicles and Their Subsystems for Virtual Reality and Mechatronics Applications $20.00
$20.00
× 3439. Weight Engineering, Loading Schedules - The 747-400 Dreamlifter Loading Schedule 3439. Weight Engineering, Loading Schedules - The 747-400 Dreamlifter Loading Schedule $20.00
$20.00
× 181. Weight Estimating Problems of Airborne Electronics Equipment 181. Weight Estimating Problems of Airborne Electronics Equipment $20.00
$20.00
× 180. Lightweight Air-Borne Electronics Made Lighter 180. Lightweight Air-Borne Electronics Made Lighter $20.00
$20.00
× 160. Weight Savings With New Magnesium Alloys 160. Weight Savings With New Magnesium Alloys $20.00
$20.00
× 172. The Weight Engineer's Approach to the Problem of Fatigue in Aircraft Structures 172. The Weight Engineer's Approach to the Problem of Fatigue in Aircraft Structures $20.00
$20.00
× 3408. On-Board Weight and Balance Application 3408. On-Board Weight and Balance Application $20.00
$20.00
× 3426. Mass Modeling Effects on Aircraft Structural Dynamics 3426. Mass Modeling Effects on Aircraft Structural Dynamics $20.00
$20.00
× 175. Operational Weight and Balance Control (Military) 175. Operational Weight and Balance Control (Military) $20.00
$20.00
× 214. A Unique Solution to the Moment of Inertia Problem 214. A Unique Solution to the Moment of Inertia Problem $20.00
$20.00
× 3409. Landing Gear Mass Prediction. A Combined Analytic and Parametric Approach 3409. Landing Gear Mass Prediction. A Combined Analytic and Parametric Approach $20.00
$20.00

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Cart totals

Subtotal $240.00
Tax $0.00
Total $240.00
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