Engineering Flight Test of the Light Observation Helicopter (LOH) OH-6A Armed (XM-27E1) and Unarmed Performance and Stability and Control

reportActive / Technical Report | Accession Number: ADA951595 | Open PDF

Abstract:

No Abstract Identified

Author(s):
Crouch, William E. ; Preisendorfer, Edward P. ; Ferrell, Kenneth R.
Author Organization(s):
ARMY AVIATION SYSTEMS TEST ACTIVITY EDWARDS AFB CA
Pagination:
0096

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Project Number(s):
67-13
Monitor Series:
USAASTA
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means; JCA_6_Net Centric; JCA_6.4.1_Secure Information Exchange; JCA_6.1.3_Switching and Routing; JCA_6.1.1_Wired Transmission; JCA_4_Logistics; JCA_5_Command and Control; JCA_6.1_Information Transport; JCA_6.4_Information Assurance; JCA_4.3_Maintain; JCA_4.6_Engineering; JCA_5.3_Planning
Communities of Interest:
Weapons Technologies
Descriptor(s):
*AERODYNAMIC STABILITY, *HELICOPTERS, *TRIM(AERODYNAMICS), AUTOROTATION, EXTERNAL STORES, FLIGHT CONTROL SYSTEMS, FLIGHT TESTING, HOVERING, LEVEL FLIGHT, MILITARY REQUIREMENTS, OBSERVATION AIRCRAFT, ROTARY WING AIRCRAFT, WEAPON SYSTEMS
Field(s)/Group(s):
Aerodynamics, Helicopters, Patrol and Reconnaissance Aircraft
Keyword(s):
OH 6A AIRCRAFT, XM 27E1 ARMAMENT SUBSYSTEMS
Report Date:
1967 Dec 01