Accession Number:

AD0625818

Title:

HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 1

Descriptive Note:

Summary rept.

Corporate Author:

HILLER AIRCRAFT CORP PALO ALTO CA

Personal Author(s):

Report Date:

1965-10-01

Pagination or Media Count:

115.0

Abstract:

The study of a tip-turbojet-powered rotor system for a heavy-lift helicopter, which is presented in thirteen volumes, is summarized. Included under this general subject are studies on parametric design, performance, structures and dynamics, wind tunnel, preliminary design, weight and balance, stability, and power plant.

Descriptors:

• *HELICOPTER ROTORS
• HELICOPTERS
• LIFT
• PERFORMANCE(ENGINEERING)
• STABILITY
• TURBOJET ENGINES
• WEIGHT

Subject Categories:

• Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE