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Accession Number:
AD0625822
Title:
HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 10. STABILITY AND CONTROL
Descriptive Note:
Engineering rept.
Corporate Author:
HILLER AIRCRAFT CORP PALO ALTO CA
Report Date:
1965-10-01
Pagination or Media Count:
90.0
Abstract:
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.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE