0

A Design Study of a Reaction Control System for a V/STOL Fighter/Attack Aircraft PUBLIC ACCESS

[+] Author Affiliations
B. B. Beard, W. H. Foley

General Dynamics Corporation

Paper No. 83-GT-199, pp. V002T02A018; 6 pages
doi:10.1115/83-GT-199
From:
  • ASME 1983 International Gas Turbine Conference and Exhibit
  • Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
  • Phoenix, Arizona, USA, March 27–31, 1983
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7952-8
  • Copyright © 1983 by General Dynamics Corporation

abstract

For all V/STOL aircraft, some type of attitude control is required in the hovering mode. In the past, this requirement has usually been met with a Reaction Control System (RCS) — a so-called “Puffer-Pipe” system which consists of high pressure gas ducted about the airframe and exhausted through nozzles at the wing tips, nose and tail.

This paper discusses a preliminary design study of an RCS for a STOVL aircraft conceptual configuration presently being developed by General Dynamics’ Fort Worth Division. The study highlights critical limitations and considerations relevant to the choice of an RCS concept. Physical requirements for RCS performance are detailed. Basic physical tradeoffs are elucidated. Various RCS candidate concepts are presented, and judged for their respective merits and drawbacks. The candidate system judged best suited for the particular application proposed is presented and discussed.

Copyright © 1983 by General Dynamics Corporation
This article is only available in the PDF format.

Figures

Tables

Interactive Graphics

Video

Country-Specific Mortality and Growth Failure in Infancy and Yound Children and Association With Material Stature

Use interactive graphics and maps to view and sort country-specific infant and early dhildhood mortality and growth failure data and their association with maternal

NOTE:
Citing articles are presented as examples only. In non-demo SCM6 implementation, integration with CrossRef’s "Cited By" API will populate this tab (http://www.crossref.org/citedby.html).

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In