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× 216. Design of Take-Off Masses of Multiple Stage, ICBM-Type Rockets With Given Range and Payload Objectives 216. Design of Take-Off Masses of Multiple Stage, ICBM-Type Rockets With Given Range and Payload Objectives $20.00
$20.00
× 147. A Rational Method for Estimating Fuel System Weight in Preliminary Design 147. A Rational Method for Estimating Fuel System Weight in Preliminary Design $20.00
$20.00
× 214. A Unique Solution to the Moment of Inertia Problem 214. A Unique Solution to the Moment of Inertia Problem $20.00
$20.00

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Subtotal $60.00
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Total $60.00