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

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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6. Flying Vehicle Control System Pneumatic Actuators / V. A. Chashhin, О. Т. Kamladze, А. B. Kondrat’yev et al. М., 1987. 248 p.
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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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