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.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
References
I. N. Zyuzin, D. B. Lempert, and G. N. Nechiporenko, Izv. Akad. Nauk, Ser. Khim., No. 6, 1354 (2003).
B. G. Trusov, in Proc. 14th Int. Symp. on Chemical Thermodynamics (Inst. of Chemistry, St.-Petersburg University, St. Petersburg, 2002), p. 483.
G. N. Nechiporenko, G. P. Dolganova, and L. N. Stesik, Khim. Fiz. 17(7), 87 (1998).
Author information
Authors and Affiliations
Corresponding author
Additional information
Original Russian Text © D.B. Lempert, G.N. Nechiporenko, S.I. Soglasnova, 2008, published in Khimicheskaya Fizika, 2008, Vol. 27, No. 12, pp. 28–32.
Rights and permissions
About this article
Cite this article
Lempert, D.B., Nechiporenko, G.N. & Soglasnova, S.I. Some anomalies in the dependence of the specific pulse of rocket propellants on the aluminum content. Russ. J. Phys. Chem. B 2, 883–887 (2008). https://doi.org/10.1134/S1990793108060055
Received:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S1990793108060055