Accession Number : AD0164468

Title :   Improved Air Generating Mechanism for an Aircraft Air Cushion Takeoff and Landing System.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Krysiak,Joseph E.

Report Date : 07 MAR 1973

Pagination or Media Count : 37

Abstract : The patent application relates to a turbine driven fan assembly containing solid rocket propellant and nozzle assemblies. The device is used to supplement the gas flow in an air cushion landing device.

Descriptors :   *Air cushion vehicles, *Landing aids, Patents, Air, Inlets, Ducts, Solid rocket propellants

Subject Categories : Surface Effect Vehicles & Amphibious Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE