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9. Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles

ISSN: 2617-5525

e-ISSN: 2617-5533

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (1); 59-66

Language: Russian

Annotation: The differential equations of the gas-jet control system two-stage hot gas distributor are considered.

Key words:

Bibliography:
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4. Mamontov M. A. Some Cases of Gas Flowing in Pipes, Heads and Flow Vessels. М., 1951. 469 p.
5. Gerz E. V., Kreinin G. V. Dynamics of Pneumatic Actuators of Automatic Machines. М., 1964. 233 p.
6. Flying Vehicle Control System Pneumatic Actuators / V. A. Chashhin, О. Т. Kamladze, А. B. Kondrat’yev et al. М., 1987. 248 p.
7. Simakov N. N. Experimental Confirmation of Early Critical Region on Single Sphere. Journal of Technical Physics. Vol. 80, Issue 7. 2010.
8. Deich М. Е. Technical Gas Dynamics. М.-L., 1961. 412 p.
9. Sitnikov B. T., Matveyev I. B. Calculation and Investigation of Safety and Relief Valves. М., 1972. 127 p.
10. Danilov Y. A., Kirillovsky Y. L., Kolpakov Y. G. Equipment of Massive Hydraulic Actuators: Operating Processes and Characteristics. М., 1990. 272 p.
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9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles
9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles
9.1.2017 Mathematical Simulation of Gas-Jet Control System Distributor for Launch Vehicles
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