SAWE Technical Papers

Showing 1921–1936 of 2068 resultsSorted by latest

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  506. STAN – A New Concept in Aircraft Weight and Balance

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  493. Weight Optimization of a Two Stage Reusable Orbital Carrier

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  491. Precise Booster Thrust Alignment in an Asymmetric Application

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  490. A Single Point Center of Gravity and Weight Measuring System for Airborne Ejection Launched Missiles

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  489. A Compression Weigh System Using the ‘Glide-Aire’ Jack Support Method

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  488. Electronic Load Cells, Their Basic Component Resistance Strain Gages

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  487. Calibration of Force Measuring Devices Utilizing Mass as a Standard

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  486. Methods of Determining Mass or Weight in a Zero-G Environment

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  480. Mass Properties Program for the 156-Inch Diameter Solid Propellant Rocket Motor

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  479. High Temperature Airframe Weight Estimation

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  478. Monte Carlo Techniques as Applied to the A3 Polaris Missile

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  477. Chemical Milling on Apollo and Saturn Gore Segments

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  476. An Approach to the Value of Weight Savings on Military Aircraft

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  475. Design and Development of a Balance Computer for the C141A (Starlifter)

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  474. On the Accuracy of the Weight Empty Estimate

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  472. Weight Estimation Methods for Frequency-Limited Support Structure

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