Fan-in-Fuselage Advanced Antitorque System

reportActive / Technical Report | Accession Number: ADA005049 | Open PDF

Abstract:

The information contained in this report is a result of study, analysis and design conducted to determine the performance of a helicopter with a fan-in-fuselage antitorque and yaw control system, as compared with the performance of the same basic helicopter with a tail rotor.

Author(s):
Akeley, Carroll R. ; Carson, George W.
Author Organization(s):
KAMAN AEROSPACE CORP BLOOMFIELD CT
Descriptive Note:
Final rept. 9 Feb 1973-31 Jan 1974
Pagination:
0101

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

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

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
USAAMRDL-TR-74-89
Contract/Grant Number(s):
DAAJ02-73-C-0033
Project Number(s):
DA-1-F-162204-AA-44
Monitor Series:
TR-74-89, USAAMRDL
 Subject Terms
Joint Capability Areas:
JCA_3_Force Application; JCA_3.1_Maneuver; JCA_3.1.1_Maneuver to Engage; JCA_6.1.3_Switching and Routing; JCA_6_Net Centric; JCA_1_Force Support; JCA_3.1.2_Maneuver to Insert; JCA_1.2_Force Preparation; JCA_5_Command and Control; JCA_1.2.6_Concepts; JCA_6.1_Information Transport; JCA_5.3_Planning; JCA_6.4.1_Secure Information Exchange; JCA_1.2.5_Lessons Learned; JCA_3.2_Engagement; JCA_3.2.1_Kinetic Means; JCA_6.4_Information Assurance; JCA_1.2.3_Educating; JCA_6.2.1_Information Sharing; JCA_6.2.2_Computing Services; JCA_4.1_Deployment and Distribution
Modernization Areas:
Directed Energy
Communities of Interest:
Energy and Power Technologies
Descriptor(s):
*DUCTED FANS, *HELICOPTERS, *TAIL HELICOPTER ROTORS, AERODYNAMIC CHARACTERISTICS, AVIATION SAFETY, MAINTAINABILITY, RELIABILITY, VULNERABILITY
Field(s)/Group(s):
Helicopters
Report Date:
1974 Nov 01