The development of two experimental burners was completed as part of a project to evaluate the suitability of the use of converted reciprocating engine turbochargers as expendable jet engines for remotely piloted vehicles. As a result of analytic studies, Burner 'A' was constructed as a reverse flow burner and was designed to accept a mass flow up to 0.75 lbm/sec. Burner 'B' was also reverse and designed for a mass flow up to 1.5 lbm/sec. Both burners operated successfully on their respective turbochargers.
Combustor design for low cost expendable turbojets
Auslegung der Brennduesen fuer unaufwendige Strahltriebwerke
US Government Reports ; 1-56
1976
56 Seiten
Report
English