Accession Number:

AD0909269

Title:

Report of the Engineering Flight Test -- Stability and Control Phase -- of the OH-5A Helicopter, Unarmed (Clean) and Armed with the XM-7 or XM-8 Weapon Subsystem. Part 1

Corporate Author:

ARMY AVIATION SYSTEMS TEST ACTIVITY EDWARDS AFB CA

Report Date:

1964-08-01

Abstract:

Stability and control tests were conducted on the OH-5A helicopter to determine stability and control characteristics throughout the flight envelope. In addition, XM-7 and XM-8 firing tests were conducted to define the aircrafts suitability for use as a weapons platform.

Supplementary Note:

See also Part 2, AD909270.

Pages:

0275

Communities Of Interest:

Modernization Areas:

Distribution Statement:

Approved for public release; distribution is unlimited. Document partially illegible.

File Size:

18.57MB