Theoretical Study on H<sub>3</sub>N<sub>3</sub>O<sub>3</sub> for Solid Rocket Propellant
Theoretical Study on H3N3O3 for Solid Rocket Propellant
Bulletin of the Korean Chemical Society. 2013. Nov, 34(11): 3189-3190
Copyright © 2013, Korea Chemical Society
  • Received : July 22, 2013
  • Accepted : August 26, 2013
  • Published : November 20, 2013
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About the Authors
Thomas M., Klapötke
Center for Energetic Concepts Development (CECD), Univ. of Maryland, College Park, MD 20742, USA
Won K., Seok
Department of Chemistry, Dongguk University, Seoul 100-715, Korea.

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Financial support of this work by the Ludwig-Maximilian University of Munich (LMU), the U.S. Army Research Laboratory (ARL), the Armament Research, Development and Engineering Center (ARDEC), the Strategic Environmental Research and Development Program (SERDP) and the Office of Naval Research (ONR) under contract nos. W911NF-09-2-0018 (ARL), W911NF-09-1-0120 (ARDEC), W011NF-09-1-0056 (ARDEC) and 10 WPSEED01-002/WP-1765 (SERDP) are gratefully acknowledged. The authors acknowledge collaborations with Dr. Mila Krupka (OZM Research, Czech Republic) and with Dr. Muhamed Suæeska (Brodarski Institute, Croatia). We are indebted to and thank Drs. Betsy M. Rice and Brad Forch (ARL, Aberdeen, Proving Ground, MD) and Mr. Gary Chen (ARDEC, Picatinny Arsenal, NJ) for many helpful and inspired discussions and support of our work.
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