Relationships Between Thrust Vectoring/Reversing Fighter Effectiveness and Air-to-Air Missile Technology

901845

09/01/1990

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
Air combat simulator studies consistently show large fighter effectiveness payoffs due to thrust vectoring and/or thrust reversing exhaust nozzles. However, the air-to-air missile related kill ratios achieved during these evaluations vary considerably as a function of maximum missile launch angle-of-attack (AOA).
This paper will review the ways thrust vectoring/reversing is used during air combat and then discuss some missile related multi-function nozzle survivability benefits. Typical air combat simulator fighter agility advantages and disadvantages attributable to vectoring/reversing nozzles will then be examined. These include relative antenna train (look) angles, capture times, and capture frequencies during close-in combat. The high AOA launch desirability will be defined along with the payoffs of attaining that capability. Nozzle max vector angles and utilization frequencies along with high AOA missile launch problems and potential solutions will also be addressed.
In addition, the relationship between pilot training and missile launch AOA will be shown as it relates to kill ratio trends.
Meta TagsDetails
DOI
https://doi.org/10.4271/901845
Pages
8
Citation
Herrick, P., "Relationships Between Thrust Vectoring/Reversing Fighter Effectiveness and Air-to-Air Missile Technology," SAE Technical Paper 901845, 1990, https://doi.org/10.4271/901845.
Additional Details
Publisher
Published
Sep 1, 1990
Product Code
901845
Content Type
Technical Paper
Language
English