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

Personal Author(s):

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.

Descriptors:

• *HELICOPTER ROTORS
• *HELICOPTERS
• CONTROL
• HANDLING
• LIFT
• PERFORMANCE(ENGINEERING)
• SPECIFICATIONS
• STABILITY

Subject Categories:

• Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE