Cart Shopping Cart My Store Account Orders Downloads Shopping Cart “2327. The Initial Weight Estimate” has been added to your cart. Continue Shopping Remove item Thumbnail image Product Price Quantity Subtotal × 2296. Center of Gravity Determination by Video Photogrammetry $20.00 2296. Center of Gravity Determination by Video Photogrammetry quantity $20.00 × 2286. Benefits of Parametric Mechanical Design Weight Scaling Decks for Advanced Aircraft Turbomachinery $20.00 2286. Benefits of Parametric Mechanical Design Weight Scaling Decks for Advanced Aircraft Turbomachinery quantity $20.00 × 315. Precision Static Center of Gravity Measurement $20.00 315. Precision Static Center of Gravity Measurement quantity $20.00 × 308. A Simplified Method for Estimating the Wetted Area of Aircraft Fuselages $20.00 308. A Simplified Method for Estimating the Wetted Area of Aircraft Fuselages quantity $20.00 × 2361. Weight Interactions With Other Attributes $20.00 2361. Weight Interactions With Other Attributes quantity $20.00 × 2349. A Light Look at a Comparison Between Empty Aircraft, Actual and Estimated Weights, for Two Time Periods: 1943-1969 & 1970 $20.00 2349. A Light Look at a Comparison Between Empty Aircraft, Actual and Estimated Weights, for Two Time Periods: 1943-1969 & 1970 quantity $20.00 × 2291. Affordable Weight Control in Today's Market $20.00 2291. Affordable Weight Control in Today's Market quantity $20.00 × 2297. Using a Spherical Air Bearing to Simulate Weightlessness $20.00 2297. Using a Spherical Air Bearing to Simulate Weightlessness quantity $20.00 × 2329. Method for Balancing VTOL/STOVL Aircraft $20.00 2329. Method for Balancing VTOL/STOVL Aircraft quantity $20.00 × 2292. F/A-18E Weight Management - Part 4 $20.00 2292. F/A-18E Weight Management - Part 4 quantity $20.00 × 2343. The Nemesis Air Racer $20.00 2343. The Nemesis Air Racer quantity $20.00 × 2287. Application of Mass Cruciforms to Finite Element Models for Inertial Representation $20.00 2287. Application of Mass Cruciforms to Finite Element Models for Inertial Representation quantity $20.00 × 2282. Semi-Analytical Method for Predicting Wing Structural Mass $20.00 2282. Semi-Analytical Method for Predicting Wing Structural Mass quantity $20.00 × 2290. New and Emerging Aluminum Products for Cost-Effective Airframe and Space Structure $20.00 2290. New and Emerging Aluminum Products for Cost-Effective Airframe and Space Structure quantity $20.00 × 2327. The Initial Weight Estimate $20.00 2327. The Initial Weight Estimate quantity $20.00 Coupon: Apply coupon Update cart Available coupons (Click to apply). Cart totals Subtotal $300.00 Tax $0.00 Total $300.00 Proceed to checkout
