Combustion considerations in fuel-rich propellant systems.
Author:
Affiliation:
1. Lockheed Propulsion Company, Redlands, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference23 articles.
1. Regression rates of nonmetalized hybrid fuel systems
2. Regression rates of metalized hybrid fuel systems.
3. Pressure dependence of hybrid fuel regression rates.
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