Loren E. Bollinger
A variable delay timer for premixed gaseous propellant rocket engines
Detonation induction distances in combustible gaseous mixtures at atmospheric and elevated initial pressures. I Methane-oxygen, II Carbon-monoxide - oxygen, III Hydrogen-oxygen
Detonation induction distances in combustible gaseous mixtures at atmospheric and elevated initial pressures. IV Hydrogen-nitric oxide, V Hydrogen-oxygen-diluent, VI Theoretical analysis
Investigation of rocket engines for the direct measurement of exhaust jet velocities
Operation and application of synchros as motion transducers in Bourdon-type gages
Research on a premixed gaseous rocket propellant
Variable pulse-width generator