Performance of Dicyclopentadiene/H2O2-Based Hybrid Rocket Motors with Metal Hydride Additives-Reference-Cited by-同舟云学术

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

Published:2013-09 Issue:5 Volume:29 Page:1122-1129
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,Pourpoint T. L.¹,Son S. F.¹,Heister S. D.¹

Affiliation:

1. School of Aeronautics and Astronautics, 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.B34867

Reference16 articles.

1. Thermal Decomposition of the Non-Interstitial Hydrides for the Storage and Production of Hydrogen

2. HumbleR. W., Space Propulsion Analysis and Design, McGraw-Hill, New York, 1995, p. 373.

3. SarnerS. F., Propellant Chemistry, Reinhold, New York, 1966, pp. 201–205.

4. GordonS. M. “Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications, Part II: User’s Manual and Program Description,” NASA RP-1311, June 1996.

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