Gas Pulsator-Pulse Jet, Fifth Partial Report
Abstract
A thrust of 298 pounds at a specific fuel value of 1.99 pounds of fuel per pound of thrust per hour was obtained with a 12-inch-diameter pulse jet 132 inches in length with step bell attached to tailpipe. Results of eleven tests of similar configurations all show values of specific fuel closely approaching 2.0. These were static tests at a mean temperature of of 27 degrees F, conducted at an elevation 100 feet above sea level.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 05, 1948
- Accession Number
- AD1207389
Entities
People
- G. C. Milak
Organizations
- United States Naval Research Laboratory