Static Thrust Augmentation Of A Rocket Ejector System With A Heated Supersonic Primary Jet
Download Static Thrust Augmentation Of A Rocket Ejector System With A Heated Supersonic Primary Jet PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Static Thrust Augmentation Of A Rocket Ejector System With A Heated Supersonic Primary Jet book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages.
Static Thrust Augmentation of a Rocket-ejector System with a Heated Supersonic Primary Jet
"An investigation was conducted in order to evaluate the static thrust augmentation attainable through the use of a rocket-ejector system with a heated supersonic primary jet. This system consisted of a cylindrical mixing tube in conjunction with a supersonic nozzle having an expansion ratio of 15 to 1. A hydrogen peroxide gas generator was used to provide heated nozzle flow. An ejector with a bellmouthed inlet provided thrust augmentation up to about 18 percent of the primary rocket thrust, whereas the use of a blunt-lip inlet with elliptical profile provided augmentation up to 9 percent. Axial withdrawal of the rocket nozzle from the ejector provided small gains in thrust augmentation."--P.[1]
Technical Publications Announcements with Indexes
Author: United States. National Aeronautics and Space Administration
language: en
Publisher:
Release Date: 1962