Zobrazeno 1 - 10
of 15
pro vyhledávání: '"V. N. Simonenko"'
Publikováno v:
Scholarly Notes of Komsomolsk-na-Amure State Technical University. 2:98-101
Autor:
R. G. Nikitin, B. V. Pevchenko, Vladimir E. Zarko, O. G. Glotov, P. I. Kalmykov, K. A. Sidorov, V. N. Simonenko, A. B. Kiskin
Publikováno v:
Combustion, Explosion, and Shock Waves. 50:306-314
The combustion behavior of high-energy systems based on furazano[3,4-e]tetrazine-4,6-dioxide and 2,4-dinitro-2,4-diazapentane with metal and energetic additives (Al, AlH3 ammonium perchlorate, ammonium dinitramide, and HMX) has been studied. The burn
Autor:
E. N. Chesnokov, K. É. Kuper, P. I. Kalmykov, Vladimir E. Zarko, A. A. Kvasov, V. N. Simonenko
Publikováno v:
Combustion, Explosion, and Shock Waves. 45:752-755
Experiments were performed to determine the threshold laser pulse energy density resulting in explosive transformation of the mixtures studied. The experiments showed the possibility of using the laser initiation technique for rapid testing of mixtur
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 8:329-344
Publikováno v:
Combustion, Explosion, and Shock Waves. 43:320-333
The combustion characteristics of propellants containing AP, HMX, an energetic binder, and aluminum particles with various polymer coatings are studied at pressures of 0.15 and 4.6 MPa. It is found that the coatings influence the burning rate, the pa
Publikováno v:
Aerospace Science and Technology. 11:13-17
The hydrazinium nitrate (N2H4∗HNO3 HN) can be considered as a candidate for using instead of ammonium perchlorate (AP) in eco-friendly solid propellant formulations. In combination with energetic binder it provides reasonably high energetic paramet
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 5:725-732
Autor:
A. B. Kiskin, V. N. Simonenko
Publikováno v:
Combustion, Explosion, and Shock Waves. 36:48-53
Combustion of condensed media results in the appearance of a recoil force of gasification products leaving the burning surface. This force is directly related to the instantaneous mass burning rate. Special features of registration of the recoil forc
Publikováno v:
Defence Science Journal. 42:183-189
The influence of constant and transient radiant flux on the burning rate of solid propellants is considered. The validity of the equivalence principle for the radiant flux and increase in initial temperature and also the problem of possible photochem
Publikováno v:
Combustion, Explosion, and Shock Waves. 33:685-687
Results of a study dealing withRDX andHMX combustion using a recoil-force transducer have been presented. Self-sustaining and radiation.-driven combustion regimes have been examined. A high-frequency (over600 Hz) component in the signal of recoil for