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×	3302. Some Considerations about Aircraft Center of Gravity	$20.00	3302. Some Considerations about Aircraft Center of Gravity quantity	$20.00
×	3322. Weight and Balance Considerations for Flight Test Aircraft On	$20.00	3322. Weight and Balance Considerations for Flight Test Aircraft On quantity	$20.00
×	3320. Static Balancing a Device with Two or More Degrees of Freedom - (The Key to Obtaining High Performance on Gimbled Missile	$20.00	3320. Static Balancing a Device with Two or More Degrees of Freedom - (The Key to Obtaining High Performance on Gimbled Missile quantity	$20.00
×	3340. Design of an Engine Inertia Measuring Device	$20.00	3340. Design of an Engine Inertia Measuring Device quantity	$20.00
×	3314. Considerations for Performing Weight Reviews and Audits	$20.00	3314. Considerations for Performing Weight Reviews and Audits quantity	$20.00
×	3300. The Value of Mass Properties Engineering	$20.00	3300. The Value of Mass Properties Engineering quantity	$20.00
×	3303. Evolutionary Feature Based Weight Prediction	$20.00	3303. Evolutionary Feature Based Weight Prediction quantity	$20.00
×	3339. Topology Optimization for Weight Reduction During Preliminary Design	$20.00	3339. Topology Optimization for Weight Reduction During Preliminary Design quantity	$20.00
×	646. STAN (R) - Integral Weight and Balance System	$20.00	646. STAN (R) - Integral Weight and Balance System quantity	$20.00
×	3317. Weights and Materials Considerations in the Design of an Ultra Heavy Lift Aircraft	$20.00	3317. Weights and Materials Considerations in the Design of an Ultra Heavy Lift Aircraft quantity	$20.00
×	3286. Developing Metal Matrix Composites For Ordnance and Aerospace Applications	$20.00	3286. Developing Metal Matrix Composites For Ordnance and Aerospace Applications quantity	$20.00
×	3331. Prediction of Fracture Damage in and Reliability Based Design Optimization of Composite Structures	$20.00	3331. Prediction of Fracture Damage in and Reliability Based Design Optimization of Composite Structures quantity	$20.00
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