Accession Number : ADA309753
Title : Unitary Joint Standoff Captive Air Training Missile Avionics Design Through Operational Concepts and Functional Requirements Analysis.
Descriptive Note : Master's thesis,
Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA
Personal Author(s) : Reilly, Dennid J., III
PDF Url : ADA309753
Report Date : MAR 1996
Pagination or Media Count : 145
Abstract : To accurately simulate the Unitary Joint Standoff (JSOW) weapon functions and provide pilots with the most realistic training, the captive air training missile (CATM) avionics design will fully implement well defined operational concepts and functional requirements in terms of flight simulation characteristics, operational functions, pilot feedback, and electronic interfaces. This would provide the Navy, Marines, and Air Force with a single, multi-capable, light weight CATM that consolidates CATM procurement, decreases aircraft turnaround time and increases aircrew training per flight hour.
Descriptors : *FLIGHT TRAINING, *AIR TO SURFACE MISSILES, WEAPONS, AVIONICS, FUNCTIONS, REQUIREMENTS, ELECTRONICS, STANDOFF, FLIGHT CREWS, INTERFACES, REACTION TIME, PILOTS, AIR FORCE TRAINING, RESPONSE, FEEDBACK, AERODYNAMIC CHARACTERISTICS, PROCUREMENT, LIGHTWEIGHT, FUNCTIONAL ANALYSIS, MARINE CORPS PERSONNEL, FLIGHT SIMULATION.
Subject Categories : Personnel Management and Labor Relations
Air- and Space-launched Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE