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
Fuels for turbojets and ramjets.
NTRS | 1964
|SMALL TURBOJETS--DESIGNS AND INSTALLATIONS
British Library Conference Proceedings | 1993
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