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HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 10. STABILITY AND CONTROL
HILLER AIRCRAFT CORP PALO ALTO CA
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The report discusses the results of a stability and control analysis of a large crane-type helicopter powered by a tip-mounted turbojet system. Specification MIL-H-8501A was used as a guide for criteria. Specification criteria were met however, for improvements in handling qualities, a stability augmentation system is recommended.
APPROVED FOR PUBLIC RELEASE