Three-Dimensionally Printed Polylactic Acid as Solid Fuel for Hydrogen Peroxide Hybrid Rockets
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Daejeon 34141, Republic of Korea
2. Delft University of Technology, 2629 HS Delft, The Netherlands
Funder
National Research Foundation of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Reference35 articles.
1. SuttonG. P.BiblarzO., Rocket Propulsion Elements, Wiley, New York, 2010, pp. 594–621, Chap. 16.
2. Regression-Rate and Heat-Transfer Correlations for Hybrid Rocket Combustion
3. Effect of swirl on the regression rate in hybrid rocket motors
4. Regression rate characteristics of hybrid rocket motor with helical grain
5. Combustion characteristics of hybrid rocket motor with segmented grain
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