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× 520. Self Improvement, Independent Action and Participation 520. Self Improvement, Independent Action and Participation $20.00
$20.00
× 524. Wing Pivot Weight Estimation Method 524. Wing Pivot Weight Estimation Method $20.00
$20.00
× 505. An Approach to an Automated System for Determination of Mass Moments of Inertia 505. An Approach to an Automated System for Determination of Mass Moments of Inertia $20.00
$20.00
× 550. A Simplified Technique for Precision Measurement of Three Axis Center of Gravity 550. A Simplified Technique for Precision Measurement of Three Axis Center of Gravity $20.00
$20.00
× 521. Weight Growth and the Principle of Minimum Contingency 521. Weight Growth and the Principle of Minimum Contingency $20.00
$20.00
× 2258. Using Microsoft Excel and Word as Weight Control Tools 2258. Using Microsoft Excel and Word as Weight Control Tools $20.00
$20.00
× 2193. Accuracy in Weighing Aircraft: Second and Third Order Effects and Techniques for Their Corrections 2193. Accuracy in Weighing Aircraft: Second and Third Order Effects and Techniques for Their Corrections $20.00
$20.00
× 2266. Affordable Thermoplastic Tailboom Structures 2266. Affordable Thermoplastic Tailboom Structures $20.00
$20.00
× 2207. Oracle Relational Database as a Mass Properties Control Tool 2207. Oracle Relational Database as a Mass Properties Control Tool $20.00
$20.00
× 2263. Army Aviation and the Mass Properties Engineer 2263. Army Aviation and the Mass Properties Engineer $20.00
$20.00
× 2228. Aircraft Cost Estimation Methodology and Value of a Pound Derivation for Preliminary Design Development Applications 2228. Aircraft Cost Estimation Methodology and Value of a Pound Derivation for Preliminary Design Development Applications $20.00
$20.00
× 2191. The Rock and Roll Telescope (Using a Gravitational Pendulum to Determine Moment of Inertia) 2191. The Rock and Roll Telescope (Using a Gravitational Pendulum to Determine Moment of Inertia) $20.00
$20.00
× 2190. Design of Fixtures for Mass Properties Measurement 2190. Design of Fixtures for Mass Properties Measurement $20.00
$20.00
× 2260. Inertia Model Database Validation at Cessna Aircraft 2260. Inertia Model Database Validation at Cessna Aircraft $20.00
$20.00

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Subtotal $280.00
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Total $280.00