Existence of limiting values of the specific impulse of metal-free composite solid propellants at a preset highest allowable combustion temperature-Reference-Cited by-同舟云学术

Existence of limiting values of the specific impulse of metal-free composite solid propellants at a preset highest allowable combustion temperature

Published:2016-07 Issue:4 Volume:10 Page:628-631
ISSN:1990-7931
Container-title:Russian Journal of Physical Chemistry B
language:en
Short-container-title:Russ. J. Phys. Chem. B

Author:

Lempert D. B.,Dorofeenko E. M.,Soglasnova S. I.,Matveev A. A.

Publisher

Pleiades Publishing Ltd

Subject

Physical and Theoretical Chemistry

Link

http://link.springer.com/content/pdf/10.1134/S1990793116040072.pdf

Reference5 articles.

1. D. B. Lempert, G. N. Nechiporenko, and S. I. Soglasnova, Combust. Explos., Shock Waves 45, 160 (2009).

2. D. B. Lempert, E. M. Dorofeenko, S. I. Soglasnova, and G. N. Nechiporenko, Combust. Explos., Shock Waves 48, 424 (2012).

3. D. B. Lempert, G. H. Hechiporenko, G. P. Dolganova, and L. N. Stesik, Khim. Fiz. 17 (7), 114 (1998).

4. B. G. Trusov, in Proceedings of the 14th International Conference on Chemical Thermodynamics (NII Khim. SPbGU, St. Petersburg, 2002), p.483.

5. D. B. Lempert, in Proceedings of the 17th International Seminar on New Trends in Research of Energetic Materials (Univ. of Parbubice, Parbubice, Czech Rep., 2014), Vol. 1, p. 281.

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Hybrid rocket propulsion technology for space transportation revisited - propellant solutions and challenges;FirePhysChem;2021-12

2. Dependence of the Temperature of the Adiabatic Transformation of Binary Mixtures of Ammonium Perchlorate and Hydrocarbon on the Enthalpy of the Latter’s Formation;Russian Journal of Physical Chemistry B;2020-09

3. Ethinyl Aromatic Hydrocarbon Derivatives as Possible Solid Fuel Dispersants;Russian Journal of Physical Chemistry B;2020-07

4. Polynitromethyl derivatives of furazano[3,4-e]di([1,2,4]triazolo)-[4,3-a:3′,4′-c]pyrazine as components of solid composite propellants;Russian Chemical Bulletin;2018-11

5. The energetic potential of azo- and azoxyfurazan nitro derivatives as components of composite rocket propellants;Chemistry of Heterocyclic Compounds;2016-12