EVALUATION OF A MECHANICAL FLIGHT CONTROL SERVO

reportActive / Technical Report | Accession Number: AD0410334 | Open PDF

Abstract:

Efforts were continued on the development of a mechanical servo for use in an all mechanical aileron flight control system for the F-100 aircraft. Detail drawings for fabrication, the installation of components, the review of a proposal ourvo, a design review mend the development progress of the toroidal servo are described.

Author(s):
No Author(s) Identified
Author Organization(s):
NORTH AMERICAN AVIATION INC LOS ANGELES CA
Descriptive Note:
Interim rept. no. 4, 1 Feb-31 Mar 1963
Supplementary Note:
DOI: 10.21236/AD0410334
Annotation:
Evaluation ofbm echanical servo for an allmechanical aileron flight control system for theF-100aircraft; Interim rept. No. 4.
Pagination:
0019

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):
NA-63-132
Contract/Grant Number(s):
NOW-62-1076
Monitor Series:
BUAER
 Subject Terms
Joint Capability Areas:
JCA_4.6_Engineering; JCA_4.6.1_General Engineering; JCA_5_Command and Control; JCA_5.3_Planning
Communities of Interest:
Air Platforms
Descriptor(s):
*FLIGHT CONTROL SYSTEMS, *JET FIGHTERS, *AILERONS, SIMULATION, SERVOMECHANISMS
Field(s)/Group(s):
Flight Control and Instrumentation, Attack and Fighter Aircraft
Keyword(s):
F 100 AIRCRAFT
Report Date:
1963 Apr 01