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Remove item	Product	Price	Quantity	Subtotal
×	2. Airplane Weight and Balance Control	$20.00	2. Airplane Weight and Balance Control quantity	$20.00
×	3. Aircraft Accessories - A Weighty Problem	$20.00	3. Aircraft Accessories - A Weighty Problem quantity	$20.00
×	26. Weight Control Organization for Manufacturers	$20.00	26. Weight Control Organization for Manufacturers quantity	$20.00
×	12. Weight Control - Aircraft Design Problem	$20.00	12. Weight Control - Aircraft Design Problem quantity	$20.00
×	33. Some Problems in the Selection of Optimum Airplane Configurations for Minimum Weight	$20.00	33. Some Problems in the Selection of Optimum Airplane Configurations for Minimum Weight quantity	$20.00
×	4. The Weight Engineer and the Flutter Problem	$20.00	4. The Weight Engineer and the Flutter Problem quantity	$20.00
×	8. A Practical Method for Wing Weight Estimation	$20.00	8. A Practical Method for Wing Weight Estimation quantity	$20.00
×	30. The Effect of Center of Gravity on Performance	$20.00	30. The Effect of Center of Gravity on Performance quantity	$20.00
×	13. Will Accessories Impede Our Payload?	$20.00	13. Will Accessories Impede Our Payload? quantity	$20.00
×	34. Pneumatic Controls for Aircraft	$20.00	34. Pneumatic Controls for Aircraft quantity	$20.00
×	15. Organization for Weight Control	$20.00	15. Organization for Weight Control quantity	$20.00
×	27. The Significance of Weight Control	$20.00	27. The Significance of Weight Control quantity	$20.00
×	35. A Graphical Method of Preparing Tabular Schedules for Balance Control in Loading Passenger Transport Aircraft	$20.00	35. A Graphical Method of Preparing Tabular Schedules for Balance Control in Loading Passenger Transport Aircraft quantity	$20.00
×	32. Weight and It's Effect on the Operation and Performance of Commercial Aircraft	$20.00	32. Weight and It's Effect on the Operation and Performance of Commercial Aircraft quantity	$20.00
×	939. Optimization of Orthotropic Layered Shells of Revolution by the Finite Element Method	$20.00	939. Optimization of Orthotropic Layered Shells of Revolution by the Finite Element Method quantity	$20.00
×	935. Weight Estimation of Hydraulic Secondary Power System	$20.00	935. Weight Estimation of Hydraulic Secondary Power System quantity	$20.00
×	938. Mass Properties History of Eccentric Insulation on a Despun Vehicle	$20.00	938. Mass Properties History of Eccentric Insulation on a Despun Vehicle quantity	$20.00
×	928. Aspects of Dynamic Balance of High RPM Spin Stabilized Rockets	$20.00	928. Aspects of Dynamic Balance of High RPM Spin Stabilized Rockets quantity	$20.00
×	931. A Moment of Gyration Concept	$20.00	931. A Moment of Gyration Concept quantity	$20.00
×	943. Spacecraft Reliability/Maintainability Optimization	$20.00	943. Spacecraft Reliability/Maintainability Optimization quantity	$20.00
×	921. Weight Control Requirements for a Prototype High Performance Craft	$20.00	921. Weight Control Requirements for a Prototype High Performance Craft quantity	$20.00
×	926. Improved Hydrostatic and Inclining Experiment Calculations for Unconventional Hull Shapes	$20.00	926. Improved Hydrostatic and Inclining Experiment Calculations for Unconventional Hull Shapes quantity	$20.00
×	934. Advanced Design Weight Prediction - Passive Thermal Protection Systems	$20.00	934. Advanced Design Weight Prediction - Passive Thermal Protection Systems quantity	$20.00
×	925. Stability and Buoyancy Criteria for Low Waterplane Catamarans	$20.00	925. Stability and Buoyancy Criteria for Low Waterplane Catamarans quantity	$20.00
×	927. The Establishment of the First SAWE Student Chapter, University of Missouri at Rolla	$20.00	927. The Establishment of the First SAWE Student Chapter, University of Missouri at Rolla quantity	$20.00
×	932. L-1011 Computerized Weight Reporting System - Present and Future Capabilities	$20.00	932. L-1011 Computerized Weight Reporting System - Present and Future Capabilities quantity	$20.00
×	923. Weight Classification Using the New Ship Work Breakdown Structure	$20.00	923. Weight Classification Using the New Ship Work Breakdown Structure quantity	$20.00
×	937. The Area Ratio Method	$20.00	937. The Area Ratio Method quantity	$20.00
×	2056. Automated Load Planning	$20.00	2056. Automated Load Planning quantity	$20.00
×	2028. The Space Exploration Initiative: Plans and Prospects	$20.00	2028. The Space Exploration Initiative: Plans and Prospects quantity	$20.00
×	2041. Weight Imjprovements in the Manufacturing Process Environment and Its Relationship to Overall Weight Control (747-400 Proc	$20.00	2041. Weight Imjprovements in the Manufacturing Process Environment and Its Relationship to Overall Weight Control (747-400 Proc quantity	$20.00
×	940. The Need for an Expanded Weight Prediction Technique	$20.00	940. The Need for an Expanded Weight Prediction Technique quantity	$20.00
×	922. Service Life Weight Control Proposal for U. S. Navy Ships	$20.00	922. Service Life Weight Control Proposal for U. S. Navy Ships quantity	$20.00
×	2050. The Boeing Model 360 Advanced Technology Demonstrator Helicopter	$20.00	2050. The Boeing Model 360 Advanced Technology Demonstrator Helicopter quantity	$20.00
×	929. Balancing Aerospace Bodies on Industrial Balancing Machines	$20.00	929. Balancing Aerospace Bodies on Industrial Balancing Machines quantity	$20.00
×	933. A New Weight Data Information System	$20.00	933. A New Weight Data Information System quantity	$20.00
×	2049. Automated Weight and Balance System	$20.00	2049. Automated Weight and Balance System quantity	$20.00
×	945. Integration of Safety Engineering Into a Cost Optimized Development Program	$20.00	945. Integration of Safety Engineering Into a Cost Optimized Development Program quantity	$20.00
×	930. Effects of Despun Masses and Aerodynamics on Dynamic Balance Error Terms	$20.00	930. Effects of Despun Masses and Aerodynamics on Dynamic Balance Error Terms quantity	$20.00
×	951. The Feasibility of the Large Freight Airship	$20.00	951. The Feasibility of the Large Freight Airship quantity	$20.00
×	963. Mass Property Calculations in SI Units	$20.00	963. Mass Property Calculations in SI Units quantity	$20.00
×	942. Ram - A Concept for Reducing Space Payload Costs	$20.00	942. Ram - A Concept for Reducing Space Payload Costs quantity	$20.00
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Subtotal	$840.00
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Total	$840.00

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