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

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.

Document Details

Document Type
Technical Report
Publication Date
Mar 07, 1973
Accession Number
AD0164468

Entities

People

  • Joseph E. Krysiak

Organizations

  • United States Department of the Air Force

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Assembly
  • Energetic Materials
  • Flow
  • Gas Flow
  • Materials
  • Patent Applications
  • Patents
  • Propellants
  • Rocket Propellants
  • Solid Rocket Propellants

Readers

  • Aerospace Engineering
  • Electrical Engineering
  • Rocket Propulsion.