Geodesic
Determination of the save distance between the carrier aircraft and launch vehicle at switch-on of the first-stage engine in air launch
Matematičeskoe modelirovanie, Tome 17 (2005) no. 11, pp. 25-42 Cet article a éte moissonné depuis la source Math-Net.Ru

Voir la notice de l'article

The emergency conditions in the air launch of the Launch Vehicle after injection from the Carrier Aircraft is considered. It is supposed that the Launch Vehicle is exploded at switch-on of the first stage engine. All factors those affect on the Carrier Aircraft are estimated. The method of the detonation wave calculation is given for solution of the two-dimensional non-stationary gas-dynamic tasks with detonation. Numerical calculations results are given those allow to determine a compromise delay of the engine switch-on. Carrier Aircraft safety and minimal payload loss are provided simultaneously. 
@article{MM_2005_17_11_a2,
     author = {Yu. G. Sikharulidze and V. A. Cherkashin and A. S. Karpov and R. K. Ivanov},
     title = {Determination of the save distance between the carrier aircraft and launch vehicle at switch-on of the first-stage engine in air launch},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {25--42},
     year = {2005},
     volume = {17},
     number = {11},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2005_17_11_a2/}
}
TY  - JOUR
AU  - Yu. G. Sikharulidze
AU  - V. A. Cherkashin
AU  - A. S. Karpov
AU  - R. K. Ivanov
TI  - Determination of the save distance between the carrier aircraft and launch vehicle at switch-on of the first-stage engine in air launch
JO  - Matematičeskoe modelirovanie
PY  - 2005
SP  - 25
EP  - 42
VL  - 17
IS  - 11
UR  - http://geodesic.mathdoc.fr/item/MM_2005_17_11_a2/
LA  - ru
ID  - MM_2005_17_11_a2
ER  - 
%0 Journal Article
%A Yu. G. Sikharulidze
%A V. A. Cherkashin
%A A. S. Karpov
%A R. K. Ivanov
%T Determination of the save distance between the carrier aircraft and launch vehicle at switch-on of the first-stage engine in air launch
%J Matematičeskoe modelirovanie
%D 2005
%P 25-42
%V 17
%N 11
%U http://geodesic.mathdoc.fr/item/MM_2005_17_11_a2/
%G ru
%F MM_2005_17_11_a2
Yu. G. Sikharulidze; V. A. Cherkashin; A. S. Karpov; R. K. Ivanov. Determination of the save distance between the carrier aircraft and launch vehicle at switch-on of the first-stage engine in air launch. Matematičeskoe modelirovanie, Tome 17 (2005) no. 11, pp. 25-42. http://geodesic.mathdoc.fr/item/MM_2005_17_11_a2/

[1] Godunov S. K. (red.), Chislennoe reshenie mnogomernykh zadach gazovoi dinamiki, Nauka, M., 1976 | MR | Zbl

[2] Korobeinikov V. P., Melnikov N. S., Ryazantsev E. V., Teoriya tochechnogo vzryva, Fizmatgiz, M., 1961 | MR

[3] Marshal V., Osnovnye opasnosti khimicheskogo proizvodstva, Mir, M., 1989

[4] Beschastnov V. A., Promyshlennye vzryvy. Otsenka i preduprezhdeniya, Khimiya, M., 1991

[5] Landau L. D., Lifshits E. M., Gidrodinamika, Nauka, M., 1986 | MR

[6] Samolet An-123-100. Rukovodstvo po letnoi ekspluatatsii, Kniga pervaya, Aviastar, U., 1993

[7] Aviatsionnye pravila. Chast 25. Normy letnoi godnosti samoletov transportnoi kategorii, LII im. M. M. Gromova, M., 1994 | Zbl