Background Information and User Guide for MIL-F-9490D

Download this report (PDF, 8.18 MB, 248 pages)
Report Number: AFFDL TR 74-116
Author(s): Townsend, James L., Raymond, Eugene T.
Corporate Author(s): Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1975-01
Pages: 248
Contract: F33615-72-C-1090
DoD Project: 8225
DoD Task:
Identifier: ADA029074

Abstract:
This document is published in support of Military Specification MIL- F-9490D, 'Flight Control Systems - Design, Installation and Test of, Piloted Aircraft, General Specification For'. It was written to aid the MIL-F-9490D user in interpretation and use of the specification. The philosophy adopted by the Air Force for this revision of MIL-F-9490 is discussed and, where pertinent, the limitations of the data or arguments used to support individual requirements are stated. Pertinent literature has also been referenced in conjunction with individual requirements, where recent supporting research and development has been accomplished.

Provenance: AFRL/VACA

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement



Export