Accession Number : AD0907289

Title :   Surface Attack Guided Missile (SAGMI) Loads Analyses.

Descriptive Note : Final rept. Feb-Dec 71,

Corporate Author : AIR FORCE ARMAMENT LAB EGLIN AFB FL

Personal Author(s) : Dyess, William W., Jr

Report Date : AUG 1972

Pagination or Media Count : 79

Abstract : This report covers the SAGMI (Surface Attack Guided Missile) to launcher interface reaction loads analysis and the SAGMI/launcher to AERO-27/F-4 interface reaction loads analyses. The basic approach used was that delineated in specification MIL-A-8591D. Several modifications to the methodology of derivation of inputs were used to simulate more accurately the conditions expected during flight. (Author)

Descriptors :   *JET FIGHTERS), (*AIR TO SURFACE MISSILES, (*LOADS(FORCES), AIR TO SURFACE MISSILES), INSTALLATION, GUIDED MISSILE LAUNCHERS, JET FIGHTERS, SWEPTBACK WINGS, FUSELAGES, FEASIBILITY STUDIES, PRESSURE, YAW, PITCH(MOTION), MANEUVERABILITY, INTERFACES, CENTER OF GRAVITY, ACCELERATION, MOMENTS, LOAD DISTRIBUTION, MATHEMATICAL ANALYSIS, SPECIFICATIONS.

Subject Categories : Attack and Fighter Aircraft
      Air- and Space-launched Guided Missiles
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE