Cart Shopping Cart My Store Account Orders Downloads Shopping Cart “22. Preliminary Design Equations for Aircraft Weight Estimation” has been added to your cart. Continue Shopping “23. The Value of a Pound” has been added to your cart. Continue Shopping Remove item Thumbnail image Product Price Quantity Subtotal × 1567. Impact of MIL-STD-1290 Crash Worthiness Requirements on Design of Helicopter Composite Structures $20.00 1567. Impact of MIL-STD-1290 Crash Worthiness Requirements on Design of Helicopter Composite Structures quantity $20.00 × 1011. A Computer Program for Parametric Sizing of Ballistic Reentry Vehicles $20.00 1011. A Computer Program for Parametric Sizing of Ballistic Reentry Vehicles quantity $20.00 × 1007. Military Specification for Weight Control Procedural Guide $20.00 1007. Military Specification for Weight Control Procedural Guide quantity $20.00 × 1032. Automated Weight Manifest - A Discussion $20.00 1032. Automated Weight Manifest - A Discussion quantity $20.00 × 1054. Motivation of Weight Engineers: A Survey $20.00 1054. Motivation of Weight Engineers: A Survey quantity $20.00 × 1570. Boeing 757-200 - Development and the Contibution of Weight and Balance Control $20.00 1570. Boeing 757-200 - Development and the Contibution of Weight and Balance Control quantity $20.00 × 15. Organization for Weight Control $20.00 15. Organization for Weight Control 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 × 27. The Significance of Weight Control $20.00 27. The Significance of Weight Control quantity $20.00 × 1047. Weight Estimation of Manned Spacecraft Metabolic Requirements $20.00 1047. Weight Estimation of Manned Spacecraft Metabolic Requirements quantity $20.00 × 14. Weight Predictor $20.00 14. Weight Predictor quantity $20.00 × 1. Weight Economy $20.00 1. Weight Economy quantity $20.00 × 34. Pneumatic Controls for Aircraft $20.00 34. Pneumatic Controls for Aircraft quantity $20.00 × 22. Preliminary Design Equations for Aircraft Weight Estimation $20.00 22. Preliminary Design Equations for Aircraft Weight Estimation quantity $20.00 × 23. The Value of a Pound $20.00 23. The Value of a Pound 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
