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Russian Journal of Physical Chemistry B

, Volume 2, Issue 6, pp 883–887 | Cite as

Some anomalies in the dependence of the specific pulse of rocket propellants on the aluminum content

  • D. B. Lempert
  • G. N. Nechiporenko
  • S. I. Soglasnova
Combustion and Explosion

Abstract

An explanation of the previously unnoticed phenomenon that the gradual introduction of aluminum into a rocket propellant composed of the C, H, N, O, and F atoms is accompanied first by a decrease in the specific impulse and then by its growth.

Keywords

Combustion Chamber Combustion Product Hydrogen Content Nozzle Exit Aluminum Content 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. 1.
    I. N. Zyuzin, D. B. Lempert, and G. N. Nechiporenko, Izv. Akad. Nauk, Ser. Khim., No. 6, 1354 (2003).Google Scholar
  2. 2.
    B. G. Trusov, in Proc. 14th Int. Symp. on Chemical Thermodynamics (Inst. of Chemistry, St.-Petersburg University, St. Petersburg, 2002), p. 483.Google Scholar
  3. 3.
    G. N. Nechiporenko, G. P. Dolganova, and L. N. Stesik, Khim. Fiz. 17(7), 87 (1998).Google Scholar

Copyright information

© MAIK Nauka 2008

Authors and Affiliations

  • D. B. Lempert
    • 1
  • G. N. Nechiporenko
    • 1
  • S. I. Soglasnova
    • 1
  1. 1.Institute of Problems of Chemical PhysicsRussian Academy of SciencesChernogolovka, Moscow oblastRussia

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