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The B-70'S New Structural Design Concepts for Mach 3 Temperatures

Published 1962-01-01 by SAE International in United States
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Evaluation of Dynamic Response Characteristics of a Supersonic Transport Landing Gear System

Published 1963-01-01 by SAE International in United States
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A Pilot's Summary of XB-70 Flight Test Experience

Published 1966-02-01 by SAE International in United States
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V/STOL Aircraft Structural Considerations

Published 1966-02-01 by SAE International in United States
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The Balanced-Power Actuation Concept

Published 1965-02-01 by SAE International in United States
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Control System Aspects of an Analytical Investigation into Controlling the Structural Modes of Flexible Aircraft

Published 1965-02-01 by SAE International in United States
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Automatic Landing Systems Mechanization - Series or Parallel Servos?

Published 1965-02-01 by SAE International in United States
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Environmental Control System Considerations for Supersonic Cruising Aircraft

Published 1965-02-01 by SAE International in United States
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Technological Advancements Resulting from XB-70 Performance Requirements

Published 1965-02-01 by SAE International in United States
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An Aircraft Manufacturer Looks at Business Aircraft Operating Costs

Published 1965-02-01 by SAE International in United States
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