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Remove item	Product	Price	Quantity	Subtotal
×	1629. Weight Control of Composite Parts in Production	$20.00	1629. Weight Control of Composite Parts in Production quantity	$20.00
×	1660. Wing Aspect Ratio Optimization Problems for Transport Turbojet Airplanes	$20.00	1660. Wing Aspect Ratio Optimization Problems for Transport Turbojet Airplanes quantity	$20.00
×	1652. The Expanded Ship Work Breakdown Structure (ESWBS) - Another Weight Classification System	$20.00	1652. The Expanded Ship Work Breakdown Structure (ESWBS) - Another Weight Classification System quantity	$20.00
×	1617. AFTI MAW - Wing of the Future	$20.00	1617. AFTI MAW - Wing of the Future quantity	$20.00
×	1661. Weight Assessment of Electronic Boxes	$20.00	1661. Weight Assessment of Electronic Boxes quantity	$20.00
×	1645. The Development of an Advanced Weight Estimation Technique for Aircraft Conceptual Design	$20.00	1645. The Development of an Advanced Weight Estimation Technique for Aircraft Conceptual Design quantity	$20.00
×	1624. Computer-Aided Controllability Assessment of Generic Manned Space Station Concepts	$20.00	1624. Computer-Aided Controllability Assessment of Generic Manned Space Station Concepts quantity	$20.00
×	25. The Effect of Overload and Unbalance on Long Range Operation	$20.00	25. The Effect of Overload and Unbalance on Long Range Operation quantity	$20.00
×	1636. Impact of Advanced Materials on Aircraft Design Weights: The Weight Improvement Factor	$20.00	1636. Impact of Advanced Materials on Aircraft Design Weights: The Weight Improvement Factor quantity	$20.00
×	1650. CAD/CAM Mass Properties	$20.00	1650. CAD/CAM Mass Properties quantity	$20.00
×	1655. Training of Mass Properties Engineers	$20.00	1655. Training of Mass Properties Engineers quantity	$20.00
×	1615. Wing Aspect Ratio Optimization Related to Payload and to Fuel Consumption of Transport Propeller Airplanes	$20.00	1615. Wing Aspect Ratio Optimization Related to Payload and to Fuel Consumption of Transport Propeller Airplanes quantity	$20.00
×	1647. An Iterative Eigenvector Approach to Determination of Prinicipal Axis Angles and Moments of Inertia	$20.00	1647. An Iterative Eigenvector Approach to Determination of Prinicipal Axis Angles and Moments of Inertia quantity	$20.00
×	1622. Conceptual Spacecraft Systems Design and Synthesis	$20.00	1622. Conceptual Spacecraft Systems Design and Synthesis quantity	$20.00
×	1609. Obtaining 3-Axis Static Balance of Gimbaled Seekers	$20.00	1609. Obtaining 3-Axis Static Balance of Gimbaled Seekers quantity	$20.00
×	22. Preliminary Design Equations for Aircraft Weight Estimation	$20.00	22. Preliminary Design Equations for Aircraft Weight Estimation quantity	$20.00
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