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