Performance and Flame Visualization of Dicyclopentadiene Rocket Propellants with Metal Hydride Additives-Reference-Cited by-同舟云学术

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Performance and Flame Visualization of Dicyclopentadiene Rocket Propellants with Metal Hydride Additives

Published:2016-07 Issue:4 Volume:32 Page:869-881
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Shark S. C.¹,Zaseck C. R.¹,Pourpoint T. L.¹,Son S. F.¹,Heister S. D.¹

Affiliation:

1. Purdue University, West Lafayette, Indiana 47907

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35853

Reference17 articles.

1. HumbleR. W., Space Propulsion Analysis and Design, 2nd ed., McGraw–Hill, New York, 1995, pp. 371–380.

2. Regression rates of metalized hybrid fuel systems.

3. COMBUSTION OF ALANE-BASED SOLID FUELS

4. Performance of Dicyclopentadiene/H2O2-Based Hybrid Rocket Motors with Metal Hydride Additives

5. Combustion of advanced non-toxic hybrid propellants

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