Accession Number:

AD0909272

Title:

Report of the Engineering Flight Test -- Performance Phase -- of the OH- 4A Helicopter, Unarmed (Clean) and Armed with the XM-7 or XM-8 Weapon Subsystem. Part 2

Descriptive Note:

Corporate Author:

ARMY AVIATION SYSTEMS TEST ACTIVITY EDWARDS AFB CA

Personal Author(s):

Report Date:

1964-08-01

Pagination or Media Count:

112.0

Abstract:

Performance flight tests were conducted on the OH-4A to determine the compliance with the Light Observation Helicopter LOH Military Characteristics and to Check the contractual guarantees outlined in the OH-4A Model Specification.

Descriptors:

• *HELICOPTERS
• AERODYNAMIC CONFIGURATIONS
• AIRCRAFT GUNS
• AIRCRAFT LANDINGS
• CENTER OF GRAVITY
• CLIMBING
• FLIGHT CONTROL SYSTEMS
• FLIGHT SPEEDS
• FLIGHT TESTING
• GRAPHICS
• GRENADES
• HANDLING
• HELICOPTER ENGINES
• HOVERING
• LEVEL FLIGHT
• PERFORMANCE(HUMAN)
• PILOTS
• PITCH(MOTION)
• ROLL
• STABILITY
• TAKEOFF
• VIBRATION
• YAW

Subject Categories:

• Helicopters
• Patrol and Reconnaissance Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE