Development of a fundamental model of hypergolic ignition in space-ambient engines.
Author:
Affiliation:
1. Polytechnic Institute of Brooklyn, Farmingdale, N. Y.
2. Thiokol Chemical Corporation, Denville, N. J.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4259
Reference7 articles.
1. Priem, R. J. and Heidmann, M. F. "Propellant vaporization as a design criterionfor rocket engine combustion chambers/' NASA TRR-67 (1960).
2. July 1965;Corbett A. D.
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