Theory of ignition of solid propellants.

Author:

PRICE E. W.1,BRADLEY H. H.1,DEHORITY G. L.1,IBIRICU M. M.1

Affiliation:

1. U. S. Naval Ordnance Test Station, China Lake, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference68 articles.

1. The concept of a condensed-phase exothermic reaction is much less plausible in an ammonium perchlorate, rubber composite propellant, and consequently attention was soon directed to models involving participation of gas-phase species in the exothermic reactions. A sequence of studies at Princeton University in the period 1956 to the present26'33included development of a "gas-phase" model in which a hot oxidizing environmental gas and fuel vapors from the propellant mixed

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