STOVL RCS Effects on Propulsion System Design

872349

12/01/1987

Event
SAE International Powered Lift Conference and Exposition
Authors Abstract
Content
Vertical landing/takeoff candidate aircraft will require some type of Reaction Control System (RCS) for aircraft balance, control, and maneuver during jet-boume flight. Typically these systems require high pressure compressor bleed air to be discharged through nozzles located on the wing tips, nose and tail of the aircraft for hover stability. Bleed rates on the order of 10 to 20 lbs/sec could be required with the source of air from compressor interstage, compression discharge or a combination from both locations.
Meta TagsDetails
DOI
https://doi.org/10.4271/872349
Pages
6
Citation
Coons, L., "STOVL RCS Effects on Propulsion System Design," SAE Technical Paper 872349, 1987, https://doi.org/10.4271/872349.
Additional Details
Publisher
Published
Dec 1, 1987
Product Code
872349
Content Type
Technical Paper
Language
English